DETAILED SYLLABUS FOR DISTANCE EDUCATION Under Graduate Degree Programs B.Tech. (Aeronautical) (SEMESTER SYSTEM) TECHNICAL CONSULTANT KCC Software Ltd. B-1/26-27,Community Center, Janakpuri. New Delhi-110058 Ph:25522801-802-803 25514608,25514534 COURSE TITLE : B.Tech(AERONAUTICAL) DURATION : 04 YEARS (Semester System) TOTAL DEGREE MARKS : 3200 FIRST SEMESTER COURSE TITLE Paper Code MARKS THEORY PRACTICAL TOTAL APPLIED MATHEMATICS-I BTAL110 100 00 100 APPLIED PHYSICS BTAL120 BTAL120/P 50 00 100 APPLIED CHEMISTRY BTAL130 BTAL130P 50 50 100 INTRODUCTION TO IT BTAL140 100 00 100 SECOND SEMESTER COURSE TITLE Paper Code MARKS THEORY PRACTICAL TOTAL PHYSICS-II BTAL210 BTAL210/P 50 50 100 CHEMISTRY-II BTAL220 BTAL220/P 50 50 100 BASICS OF ELECTRICAL ENGINEERING BTAL230 100 00 100 PROGRAMMING IN 'C' BTAL240 BTAL240/P 50 50 100 THIRD SEMESTER COURSE TITLE Paper Code MARKS THEORY PRACTICAL TOTAL FLIGHT MECHANICS BTAL310 100 00 100 THERMODYNAMICS BTAL320 100 00 100 FLUID MECHANICS BTAL330 BTAL330P 50 50 100 AIRCRAFT PRODUCTION BTAL340 100 00 100 FOURTH SEMESTER COURSE TITLE Paper Code MARKS THEORY PRACTICAL TOTAL MEASUREMENTS AND INSTRUMENTATION BTAL410 BTAL410P 50 50 100 AEROSPACE STRUCTURES I BTAL420 100 00 100 BTAL430 BTAL430P 50 50 100 AEROSPACE STRUCTURE BTAL440 100 100 100 FIFTH SEMESTER COURSE TITLE Paper Code MARKS THEORY PRACTICAL TOTAL FLIGHT MECHANICS BTAL510 BTAL510P 50 50 100 SYSTEM MODELLING AND DYNAMICS BTAL520 100 00 100 CONTROL THERAPY BTAL530 100 00 100 AIRCRAFT PROPULSION BTAL540 BTAL540P 50 50 100 SIXTH SEMESTER COURSE TITLE Paper Code MARKS THEORY PRACTICAL TOTAL AERODYNAMICS LABORATORY BTAL610 100 00 100 AIRCRAFT STRUCTURE LABORATORY BTAL620 100 00 100 AERODYNAMICS OF AEROSPACE VEHILES BTAL630 100 00 100 AEROSPACE STRUCTURES III BTAL640 BTAL640P 50 50 100 SEVENTH SEMESTER COURSE TITLE Paper Code MARKS THEORY PRACTICAL TOTAL MECHANICS AND MACHINE DESIGN BTAL710 100 00 100 COMPUTATIONAL FLUID DYNAMICS BTAL720 100 00 100 AIRCRAFT DESIGN BTAL730 BTAL730P 50 50 100 CONTROL SYSTEMS LABORATORY BTAL740 100 00 100 EIGHTH SEMESTER COURSE TITLE Paper Code MARKS THEORY PRACTICAL TOTAL SPACE LIGHT MACHANICS BTAL810 100 00 100 INTRODUCTION TO COMPOSITE STRUCTURES BTAL820 100 00 100 ELECTIVE BTAL830 -- -- 100 PROJECT BTAL840 -- -- 100 ELECTIVE (SELECT ANY ONE) COURSE TITLE Paper Code MARKS THEORY PRACTICAL TOTAL DYNAMICAL SYSTEM E1 BTAL-840 E1 BTAL-840P 50 50 100 GAS DYNAMICS E 2 BTAL-840 100 00 100 Note: Theory Paper: 40% Continuous Internal Assessment and 60 % University examination. Practical Paper: 40 % Continuous Internal Assessment and 60 % University examination. Continuous Internal Assessment: 1) Two or three tests out of which minimum 60% of Continuous Internal Assessment Two will be considered for Assessment 2) Seminars/Assignments/Quizzes 30% of Continuous Internal Assessment 3) Attendance, class participation 10% of Continuous Internal Assessment And behavior FIRST SEMESTER BTAL-110 APPLIED MATHEMATICS -I Maximum Time :3 Hrs. University Examination : 60 Marks Total Marks :100 Continuous Internal Assessment : 40 Marks Minimum Pass Marks :40% A) Instructions for paper-setter 1. The question paper will consist five sections namely A, B, C, D and E. 2. Each of the sections A, B, C and D will contain two questions and candidates have to attempt at least one question compulsorily from each section. Each section carry 15% of the total marks 3. Section E will comprise of 10-15 short answers type questions, which will cover the entire syllabus and will carry 40% of the total marks. B) Instructions for candidates 1. Candidates are required to attempt one question each from sections A, B, C and D of the question paper and the entire section E. 2. Use of non-programmable scientific calculator is allowed. SECTION A Calculus of Functions of One Variable: Successive Differentiation, Leibnitz's theorem (without proof). Mean value theorem, Taylor's theorem, Remainder theorem, Asymptotes, Curvature. Infinite Series: Convergence, divergence, Comparison test, Ratio test, Cauchy Leibnitz's theorem (without proof), Absolute and Conditional Convergence. Taylor and Maclaurin series, Power Series, Radius of Convergence. Integral Calculus: Fundamental theorems, Reduction Formulae, Properties of definite Integral, Applications of length, area, volume, surface of revolution, moments, center of gravity. Improper integrals, Beta-Gamma functions, Numerical Integration using Trapezoidal and Simpson's rules. Calculus of Functions of Several Variables Partial derivatives, Chain rule, Differentiation of Implicit functions, Exact differentials. Tangents and Normals, Maxima, Minima and Saddle points. Method of Lagrange multipliers, Errors and Approximations, Differentiation under integral sign Jacobians and transformations of coordinates. Multiple Integrals-Double and Triple integrals. Applications to areas, volumes etc. SECTION B Ordinary Differential Equations: Formation of ODE's, definition of order, degree and solutions. ODE's of first order: Method of separation of variables, homogeneous and nonhomogeneous equations, exactness and integrating factor General linear ODE's of the nth Order: solution of homogeneous and non homogeneous equations, operator method, method of undetermined coefficients and variation of parameters. Solutions of simple simultaneous ODE's . SECTION C Inner product spaces, Matrices and determinates, Linear transformations. Systems of linear equations-consistency and inconsistency, Hermitian, Skew-Hermitian Forms, Eigenvalues and Eigenvectors of matrix, diagonalization of a matrix, Cayley-Hamilton Theorem (without poof) Complex Variables: Curves and Regions in the Complex Plane, Complex Functions, Limits, Derivative, Analytic Function, Cauchy-Riemann Equations, Laplace's Equation, Rational, Exponential, Trigonometric, Hyperbolic Function's Linear Fractional Transformations, Conformal Mapping, Complex Line Integral, Cauchy's Integral Theorem, Cauchy's Integral Formula, Derivatives of Analytic Function, Power Series, Taylor Series, Laurent Series. Methods for obtaining Power Series, Analyticity at Infinity, Zeroes, Singularities, Residues, Residue Theorem, Evaluation of Real Integrals. SECTION D Vector Calculus: Scalar and vector fields, Curves, Arc length, Tangent, Directional Derivative, gradient of Scalar field, divergence and curl of a vector field. Line integrals (independent of path,) Green's theorem, Divergence theorem and Stoke's theorem (without proofs), Surface Integrals. Probability and Statistics : Random Variables, Discrete and Continuous Distribution, Mean and Variance of a Distribution, Moment Generating Functions, Skewness, Kurtosis, Binomial, Poisson, Normal Distributions, Testing of Statistical Hypothesis, F Test, T-Test, X2 test. BTAL-120 APPLIED PHYSICS Maximum Time : 3 Hrs. University Examination : 30 Marks Total Marks : 50 Continuous Internal Assessment : 20 Marks Minimum Pass Marks : 40% A) Instructions for paper-setter 1. The question paper will consist five sections namely A, B, C, D and E. 2. Each of the sections A, B, C and D will contain two questions and candidates have to attempt at least one question compulsorily from each section. Each section carry 15% of the total marks 3. Section E will comprise of 10-15 short answers type questions, which will cover the entire syllabus and will carry 40% of the total marks. B) Instructions for candidates 1. Candidates are required to attempt one question each from sections A, B, C and D of the question paper and the entire section E. 2. Use of non-programmable scientific calculator is allowed. SECTION A Kinematics: Need of frames of reference in describing motion, One Dimensional motion, Two Dimensional motion Dynamics: Central forces, Inverse square force, Satellite including applications in remote sensing and communication. Oscillations, General potential with stable equilibrium point, Solution of differential equation with emphasis on initial conditions, Damped and forced oscillations. Waves: Waves on a stretched string, Differential equation of wave, Description of general solution f(x+vt) Longitudinal and transverse waves, Superposition of waves, Plane monochromatic waves, m =nD , plane, spherical and cylindrical wavefronts. Pressure equation, decibel, reverberation, ultrasonic SECTION B Optics: Optical Instruments – Telescope, Microscope, Radio Telescope, Electron Microscope. Interference of light – Newton's rings, testing of flatness, curved surfaces, alignment. Diffraction, Resolution, Polarisation with application Principle of laser, design of laser, stimulated radiation, population inversion, laser action, properties and application of laser light. Modern physics: Theory of Relativity Elements of Quantum Mechanics including atomic spectra, X-rays, Ultrasound, Infrared radiations, Nuclear radiations and detectors. SECTION C Heat: Temperature measurement and controls, Resistance thermometer, thermo emf, high and Low temperature measurements, thermistor, thermostatic and other temperature control devices. Black body radiation, Kirchoff's Law, Stefan-Boltzman's Law, Wien's Law, Rayleigh jeans's Law, Planck's Law. Ultrasonic: Piezo-electric effect, production-(using Quartz, Ceramics and Magnetostriction), Detection, velocity measurement and application of ultrasonic waves (cavitations, thickness, Echo, chemical reactions). Motion of charged particle in Electric and magnetic fields. Magnetic and electrostatic focussing, Determination of e/m by cathode ray tube, Functions and block diagram of CRO Positive rays, Thomson parabolic method, Isotopes, Mass spectrograph (Aston and Bainbridge). Cyclotron. Semiconductors and Electronics: Characteristics of p-n junction, static and dynamic resistance, Zener diode and LED, diode as a rectifier, Transistor (pnp and npn) characteristics, Current and voltage gain. SECTION D Solid State Physics: Crystal structures, X-Ray diffraction, Superconductivity, Meissner effect, London Equation, BCS theory, Properties and applications of super conductors. Fibre Optics: Type of fibres, step index and graded index, Numerical aperture, Uses of Optical fibres in communication. Heisenberg uncertainty principle, de Broglie's hypothesis (matter waves), Davisson and Germer expt., Development of Schrodinger wave equation, solution of the Sch. Wave eqn for free and bound state, Sch. Wave eqn applied to Metals & Semiconductors, Vector atomic model, Pauli's spin quantum numbers, Stem Garlach expt, Electro-optical Effect (Stark effect), Magneto-optical effect (Zeeman effect) Basic introductory concepts of creation of Universe: Big Bang, Steady state, Pulsating state, Quasars, Pulsars, Black hole BTAL-120 P APPLIED PHYSICS Maximum Time : 3 Hrs. University Examination : 30Marks Total Marks : 50 Continuous Internal Assessment : 20 Marks Minimum Pass Marks : 40% Measurement of short time intervals using electronic timer sensors. Study of rotational motion of cycle wheel Study of oscillatory systems Study of stationary waves Use of prism spectrometer Measurement of wavelength of light by bi-prism/Newton rings/Diffraction grating Diffraction of light using Sodium source and Helium Neon source. Study of polarization of light Study of laser parameters/diffraction at a circular aperture Experiment on Ultrasonic. Heat: Platinum resistance thermometer, Calibration of thermocouple, Lee's method, Stefan's Constant, Emissive Power. Optics: Dispersive power of prism, Polarization, He-Ne Laser, fibre optics, Diffraction grating, Newton's rings Sound: Ultrasonic, to find ultrasonic velocity in different materials, ultrasonic diffraction grating Measurement of resistances of various orders, AC and DC voltages using digital millimeters. Measurement of voltage, and frequencies of AC waveform from a function generator using CRO, formation of Lisajous figure. Determination of e/m by J.J. Thomson's method Charging and discharging Measurement of thermo emf between different types of thermocouples as a function of temperature difference between the junction, measurement of an unknown temperature Design and use of potentiometer Use of Carey Foster bridge. The laboratory course will comprise of exercises on what is learnt in the theory classes of the same course i.e. BTAL 120. BTAL 130 APPLIED CHEMISTRY Maximum Time : 3 Hrs. University Examination : 30Marks Total Marks : 50 Continuous Internal Assessment : 20 Marks Minimum Pass Marks : 40% A) Instructions for paper-setter 1. The question paper will consist five sections namely A, B, C, D and E. 2. Each of the sections A, B, C and D will contain two questions and candidates have to attempt at least one question compulsorily from each section. Each section carry 15% of the total marks 3. Section E will comprise of 10-15 short answers type questions, which will cover the entire syllabus and will carry 40% of the total marks. B) Instructions for candidates 1. Candidates are required to attempt one question each from sections A, B, C and D of the question paper and the entire section E. 2. Use of non-programmable scientific calculator is allowed. SECTION A Water : Specifications for water, Analysis of water-Alkalinity, hardness and its determination (EDTA Method only), water for domestic use, Water-softening-Lime-Soda process, Ion exchangers polished water, Boiler-feed water, boiler problems-scale, sludge, priming and foaming, caustic embrittlement and corrosion, their causes and prevention, removal of silice, removal of dissolved gases, carbonates phosphate conditioning, colloidal conditioning, Calgon treatment, conditioning, Numerical problems of Alkalinity, hardness Lime-Soda process and EDTA method. Fuels : Definition and classification, combustion and chemical principles involved in it. Calorific value : Gross and net Calorific values and their determination by Buoy's Gas Calorimeter and Bomb Calorimeter. Solid Fuels : Proximate and ultimate analysis of coal and their importance. Carbonization: High and Low temperature carbonization, coke, its manufacture by Otto Hoffman Oven and uses. Liquid Fuels: Conversion of coal into liquid fuels (Bargius process and Fischer Tropsch Process and mechanism, Petroleum: its Chemical composition and Fractional distillation, Cracking of heavy oil residues : thermal cracking and catalytic cracking, knocking-chemical structure and knocking : Octane and Cetane number and their significance, Power alcohol. Gaseous Fuels: Natural gas, producer gas, water gas, carbureted water gas, coal gas and oil gas, fuel and fuel gases and their analysis by Orsat's apparatus. Numerical on calorific value, combustion, Proximate and ultimate analysis of coal and fuel gas analysis. Nuclear Fuels: Nuclear reaction, nuclear fission and nuclear fusion, Nuclear reactor SECTION B Transition Elements: General Properties with special reference to electronic configuration colour and magnetic properties of transition metal compounds. Inorganic Polymers: Types of polymers, Phosphazenes, polysiloxanes and sulphur containing polymers-their structures and properties Solutions : Ideal and non ideal solutions Raoult's Law. Distillation of binary solutions. Henry's Law, Nernst distribution law, Arrenius theory and special behavior of strong electrolytes. SECTION C Chemical Bonding: Ionic bond energy changes, lattice energy Born Haber Cycle, Covalent bond-energy changes, Potential energy curve for H2 molecule, characteristics of covalent compound, co-ordinate bond-Werner's Theory, effective atomic numbers, isomerism in coordinate compounds. Hydrogen bonding, Vander Waal's forces, hybridization and resonance, Valence Shell Electron Repulsion theory (VSEPR). Discussion of structures of H2O, NH3, BF3 SiF4, Molecular orbital theory, Linear combination of atomic orbitals (LCAO) method. Structure of simple homo nuclear diatomic molecule like H2, N2, O2, F2 Gaseous State: Gas Laws and kinetic theory of gases, Distribution of Molecular velocities, mean free path. Real gases-non ideal behaviours, Causes of deviation from ideal behaviour Vander Waal's equation. Liquefaction of gases. Thermochemistry: Hess's Law, heat of a reaction, effect of temperature on heat of reaction at constant pressure (Kirch off's Equation), heat of dilution, heat of hydration, heat of neutralization and heat of combustion, Flame temperature. SECTION D Catalysis: Criteria for Catalysis- Homogeneous Catalysis, acid-base, Enzymatic catalysis, Catalysis by metal salts, Heterogeneous Catalysis-concepts of promoters, inhibitors and poisoning, physiosorption, Chemisorption, Surface area, Industrially important process, Theories of Catalysis. Plastic: Thermosetting and Thermoplastic, properties and applications. Conducting Polymer- properties and application. Composites: Classification, micro-mechanics of fibre and particle reinforced composites, strength, stiffness and factors affecting failure modes. BTAL 130 P APPLIED CHEMISTRY Maximum Time : 3Hrs. University Examination : 30Marks Total Marks : 50 Continuous Internal Assessment : 20 Marks Minimum Pass Marks : 40% To determine the percentage composition of a mixture of Sodium hydroxide and Sodium chloride. To determine the amount of Sodium Carbonate in the given mixture of Sodium Carbonate and Sodium bicarbonate. Determine the amount of oxalic acid and Sulphuric acid/Hydrochloric acid in one litre of solution given standard sodium hydroxide and Potassium per magnate. To determine the carbonate, bicarbonate and chloride contents in irrigation water. To determine the number of water molecules of crystallization in Mohr salt provided standard dichromate solution using internal indicator. Determine the amount of Cu in the copper ore solution provided hypo solution Iodiomatic titration of K2Cr2O7 V/S Na2S2O3 to determine the percentage purity of K2Cr2O7 sample. Argentometric titration one each of Vohlard's method and of Mohr's method. Determination of dissolved oxygen in the given sample of water Determine the surface tension of a liquid using drop weight method. Determine the heat of hydration of CuSO4..5H2O/FeSO4, 7H2O Determine the heat of neutralization of Strong Acid (say H2SO4/HCI) with strong base NaOH Determine the heat of Weak Acid with strong base Determine the molecular weight of a substance by Rast method Determination of reaction rate constant for a Ist Order reaction Complexometric titrations To determine the viscosity of the given liquid (density also to be determined) Preparation of Polymer To determine the cell constant of a conductivity cell Titration of strong acid/strong base conductometrically. BTAL-140 INTRODUCTION TO IT Maximum Time : 3 Hrs. University Examination : 60Marks Total Marks : 100 Continuous Internal Assessment : 40 Marks Minimum Pass Marks : 40% A) Instructions for paper-setter 1. The question paper will consist five sections namely A, B, C, D and E. 2. Each of the sections A, B, C and D will contain two questions and candidates have to attempt at least one question compulsorily from each section. Each section carry 15% of the total marks 3. Section E will comprise of 10-15 short answers type questions, which will cover the entire syllabus and will carry 40% of the total marks. B) Instructions for candidates 1. Candidates are required to attempt one question each from sections A, B, C and D of the question paper and the entire section E. 2. Use of non-programmable scientific calculator is allowed. SECTION A An Overview of the Computer System-The Processor (CU, ALU) Factors affecting processor speed, The Bus-Data Bus and Address Bus. Memory (RAM, ROM, Registers, Cache). SECTION B I/O Devices (Mouse, Keyboard, Monitors, Printers, Pens, Touch Screens, Microphones and Voice Recognition), Storage Devices (Diskettes, Hard Disc, CD-ROM). Computer Categorization. SECTION C Networks-Uses, Categories & Topologies. System software and Application Software, Operating System-User Interface, Resource Management, Utility Software. Word Processing and Desktop Publishing, Spreadsheets & Basics of Database Management. SECTION D Programming Language: High level language, Low Level Language & Assembly Language. Major Features of the Internet, Working with Graphics, Types of Information Systems & System Development Life Cycle. SECOND SEMESTER BTAL-210 PHYSICS -II Maximum Time : 3 Hrs. University Examination : 30Marks Total Marks : 50 Continuous Internal Assessment : 20 Marks Minimum Pass Marks : 40% A) Instructions for paper-setter 1. The question paper will consist five sections namely A, B, C, D and E. 2. Each of the sections A, B, C and D will contain two questions and candidates have to attempt at least one question compulsorily from each section. Each section carry 15% of the total marks 3. Section E will comprise of 10-15 short answers type questions, which will cover the entire syllabus and will carry 40% of the total marks. B) Instructions for candidates 1. Candidates are required to attempt one question each from sections A, B, C and D of the question paper and the entire section E. 2. Use of non-programmable scientific calculator is allowed. SECTION A Waves and particles : Inadequecy of classical mechanics - wave and particle duality of radiation - de Broglie's concept of matter waves - properties of matter waves - properties of matter waves - Heisenberg's uncertainity principle - Schrodinder's wave equation ( time independent ) - physical interpretation of the wave equation - particle enclosed in one dimensional potential well of infinite hieght SECTION B Crystal structure :Crystal structure - crystal systems - bravias lattice - Miller indices - atomic radius - cordination number - atomic packing factor calculation - X-ray diffraction - phase problem and solving methods - powder photograph method SECTION C Dielectric materials :Free electron theory - band theory of the solids(elementary ideas) - metals, semiconductors and insulators - dielectric materials - -definitions - types of polarisation - internal field - Lorentz equation - Claussius-Mossetti equation - Frequency dependance - ferroelectric materials SECTION D Magnetic materials and super conductivity : Magnetis materials - definitions - types and properties - domain structure - hard and soft magnetic materials - applications - ferrites superconductivity - temperature dependence of resistance - Meissner effect - properties - explanation - BCS theory ( Basic ideas ) - types of semiconductors - High temperatre Semiconductors - Applications. Nonlinear systems and circuits :Introduction to Nonlinear dynamical systems - examples - linear systems - superposition principle - linear harmonic oscillator - free, damped and forced vibrations - resonance - duffing oscillator ( cubic nonlinear oscillator ) - LCR circuit - nonlinear electronic circuits - applications. BTAL-210 P PHYSICS -II Maximum Time : 3 Hrs. University Examination : 30Marks Total Marks : 50 Continuous Internal Assessment : 20 Marks Minimum Pass Marks : 40% 1. Determination of wavelength using grating - spectrometer 2. Determination of optical obsorption coefficient of material using Laser 3. Determination of numerical aperture and attunation coefficent of an optical fiber 4. Calibration of Ammeter-potentiometer 5. Measurement of temperature using thermocouple 6. Non-destructive testing by Ultrasonic method 7. Characteristics of a temperature sensor BTAL-220 CHEMISTRY Maximum Time : 3 Hrs. University Examination : 30Marks Total Marks : 50 Continuous Internal Assessment : 20 Marks Minimum Pass Marks : 40% A) Instructions for paper-setter 1. The question paper will consist five sections namely A, B, C, D and E. 2. Each of the sections A, B, C and D will contain two questions and candidates have to attempt at least one question compulsorily from each section. Each section carry 15% of the total marks 3. Section E will comprise of 10-15 short answers type questions, which will cover the entire syllabus and will carry 40% of the total marks. B) Instructions for candidates 1. Candidates are required to attempt one question each from sections A, B, C and D of the question paper and the entire section E. 2. Use of non-programmable scientific calculator is allowed. SECTION A Phase rule: Statement of the phase rule - Explanation of the terms - one component systems - Water and sulphur systems - Two component alloy systems - Thermal analysis - Eutectics - Lead-silver system - Application of eutectics - Compound formation - Zn-Mg system - Two components forming solid solutions. SECTION B Water treatment: Hard and soft water - Estimation of hardness by EDTA - ppm - Softening of water - Zeolite process,lime soda process and demineralisation by ion exchangers - boiler feed water, it's specification - Treatment of water for domestic purposes - Desalinisation - Reverse osmosis and electrodialysis . SECTIONC Pollution and waste water treatment : Definition - Sources - Types of air and water pollutants - BOD and COD - Treatment of domestic waste water - Composition of effluents from textiles,tannery and oil refinery industries - Their harmful effects - Radioactive wastes - Methods of containment. SECTION D Fuels : Fuels - Classification - Examples and relative merits - Types of coal - Proximate and ultimate analysis of coal Petroleum - Origin - Refining - fractional distillation - Cracking - Polymerisation process - Knocking - Leaded petrol - Octane and Cetane numbers lubricants :Definition and theories of lubrication - Charecteristics of lubricants - Viscousity, viscousity index, oiliness, pour point, cloud point,flash point,fire point and carbon residue - Additives to lubricants, manufacture of lubeoil - Synthetic lubricants - Greases - Solid lubricants BTAL-220P CHEMISTRY Maximum Time : 3 Hrs. University Examination : 30Marks Total Marks : 50 Continuous Internal Assessment : 20 Marks Minimum Pass Marks : 40% 1. Carbonate and Non-Carbonate hardness of water 2. Alkalinity of water 3. Total hardness of water 4. Estimation of Fe3+ using spectroclorimeter 5. Viscousity determination using Red wood viscometer 6. Calorific value of a fuel using the Bomb calorimeter 7. Aniline point of a lubricant 8. Flash and power points of a lubricant 9. Proximate analysis of coal BTAL-230 BASICS OF ELECTRICAL ENGINEERING Maximum Time : 3 Hrs. University Examination : 60Marks Total Marks : 100 Continuous Internal Assessment : 40 Marks Minimum Pass Marks : 40% A) Instructions for paper-setter 1. The question paper will consist five sections namely A, B, C, D and E. 2. Each of the sections A, B, C and D will contain two questions and candidates have to attempt at least one question compulsorily from each section. Each section carry 15% of the total marks 3. Section E will comprise of 10-15 short answers type questions, which will cover the entire syllabus and will carry 40% of the total marks. B) Instructions for candidates 1. Candidates are required to attempt one question each from sections A, B, C and D of the question paper and the entire section E. 2. Use of non-programmable scientific calculator is allowed. SECTION A Dc & ac circuits : Direct currents and voltages - power - DC circuits - Kirchoff's laws - alternating currents and voltages - peak, average and RMS values - circuit elements R L & C - phasors - Phasor diagrams - impedence - Real and Reactive power - Single phase and Three phase balanced AC circuits - star and delta connected loads - power measurement using two watt meter method SECTION B Dc machines and transformers : Construction and Principle of operation of DC Generators and motors - Different types - EMF equation - Characteristics of DC motors - applications - construction and principle of operations of transformers SECTION C Synchronous, induction and special machines : Construction and Principle of operation of Alternators, Synchronous motors, Three phase and Single Phase Induction motors, Stepper motors and servo motors - Elementary ideas of Power systems. SECTION D Semiconductor devices : Electrical conduction in intrinsic and extrinsic semiconductors - PN junction - principle of operation and characteristics of semiconductor diode - Bipolar Junction Transistors - FET and MOSFET - Application as amplifier and switch - CMOS switch BTAL-240 PROGRAMMING IN 'C' Maximum Time : 3 Hrs. University Examination : 60Marks Total Marks : 100 Continuous Internal Assessment : 40 Marks Minimum Pass Marks : 40% A) Instructions for paper-setter 1. The question paper will consist five sections namely A, B, C, D and E. 2. Each of the sections A, B, C and D will contain two questions and candidates have to attempt at least one question compulsorily from each section. Each section carry 15% of the total marks 3. Section E will comprise of 10-15 short answers type questions, which will cover the entire syllabus and will carry 40% of the total marks . B) Instructions for candidates 1. Candidates are required to attempt one question each from sections A, B, C and D of the question paper and the entire section E. 2. Use of non-programmable scientific calculator is allowed. SECTION A Information technology:- Information Technology - Hardware and Software - CPU Input/ Output devices - Memory & Storage - Operating System - Low level languages - Highlevel languages - Flow charts and Pseudocodes SECTION B Introduction to c :- 'C' Language - Character Set - Identifiers and keywords - Datatypes - Statements - Operators - Arithmetic, Unary, Relational, Logical, Assignment, Conditional Operators - Precedence of Operators -Input and output functions - Library functions SECTION C Control statements and arrays :-Branching, Lopping, nested control structures - Multiway branch - break - continue statements - Unconditional transfer - Arrays, Definition, Processing. SECTION D Functions and storage classes :-Defining and assessing a function - Passing arguments to a function - Recursion - Storage Classes: Auto, Extern, Register and Static - Multi file programs Pointers Pointer declarations - Pointers and one dimensional, multi-dimensional arrays - Dynamic memory allocation - Operations on pointers - Arrays of pointer BTAL-240P PROGRAMMING IN 'C' Maximum Time : 3 Hrs. University Examination : 30Marks Total Marks : 50 Continuous Internal Assessment : 20 Marks Minimum Pass Marks : 40% PRACTICALS Basic DOS Commands - Introduction to MS-word - 'C' Programming practice ( 10-12 exercises ) THIRD SEMESTER BTAL-310 FLIGHT MECHANICS 1 Maximum Time : 3 Hrs. University Examination : 60 Marks Total Marks : 100 Continous Internal Assessment : 40 Marks Minimum Pass Marks: 40% A) Instructions for paper-setter 1. The question paper will consist five sections namely A, B, C, D and E. 2. Each of the sections A, B, C and D will contain two questions and candidates have to attempt at least one question compulsorily from each section. Each section carry 15% of the total marks 3. Section E will comprise of 10-15 short answers type questions, which will cover the entire syllabus and will carry 40% of the total marks. B) Instructions for candidates 1. Candidates are required to attempt one question each from sections A, B, C and D of the question paper and the entire section E. 2. Use of non-programmable scientific calculator is allowed. SECTION A Nomenclature of aircraft components. Standard atmosphere. Basic Aerodynamics : Streamlines, steady fluid motion, incompressible flow, Bernoulli"s equation,Mach number. SECTION B Pressure and airspeed measurement, Boundary Layer,Reynolds number, Laminar and Turbulent flow. Airfoils and wings: pressure coefficient and lift calculation, Critical Mach number, Wave drag, Finite wings, Induced drag, Swept wings. SECTION C Aircraft performance: steady level flight, Altitude effects, Absolute ceiling, steady climbing flight, Energy methods, Range and Endurance, Sustained level turn, pull-up, V-n diagram SECTION D Take off and landing. Reentry vehicles: Ballistic and Glide Reentry, Blunt body concept. REFERENCES 1. Ojha S.K., Flight Performance of Aircraft, AIAA Series, 1995. 2. Anderson, J.D., Introduction to Flight, McGraw Hill, 1989. 3. Hale, J.F., Introduction to Aircraft Performance, Selection and Design, John Wiley, 1984 BTAL-320 THERMODYNAMICS Maximum Time : 3 Hrs. University Examination : 60 Marks Total Marks : 100 Continous Internal Assessment : 40 Marks Minimum Pass Marks: 40% A) Instructions for paper-setter 1. The question paper will consist five sections namely A, B, C, D and E. 2. Each of the sections A, B, C and D will contain two questions and candidates have to attempt at least one question compulsorily from each section. Each section carry 15% of the total marks 3. Section E will comprise of 10-15 short answers type questions, which will cover the entire syllabus and will carry 40% of the total marks. B) Instructions for candidates 1. Candidates are required to attempt one question each from sections A, B, C and D of the question paper and the entire section E. 2. Use of non-programmable scientific calculator is allowed. SECTION A Basic concepts :Scope and Method of Thermodynamics; System-Boundary, Surroundings; State, Stable Equilibrium, State Co-ordinates and parameters, Extensive and Intensive Parameters; Energy interactions,Work and Heat transfers, Equilibrium, Quasistatic and Reversible process, SECTION B Non-equilibrium and Irreversible Processes; Zeroth Law and Temperature, First Law and Internal Energy; Second Law - Entropy and Absolute Temperature; Third Law and Absolute Entropy;Thermodynamics of simple compressible systems, State postulate, Fundamental Representations SECTION C Thermodynamic Potentials; Jacobeam and Legender Transformations - Maxwell"s Equations, Derivation of thermodynamic properties. Applications: Closed and open systems, Polytropic processes, Cyclic process - Carnot"s cycle; Gas and vapour power cycles; Gas and vapour Refrigeration cycles; SECTION D Operating Hardware of Engines; Mixtures of gases and vapours, Elements of Combustion; Elements of Heat Transfer, One-D compressible flow, isentropic flow, flow with friction and heat transfer, normal shock. Introduction to Aerospace power plants. REFERENCES 1. Nag, P.K. Engineering Thermodynamics, Tata McGraw Hill Co., 1989 . 2. Emmanuel G., Advanced Classical Thermodynamics, AIAA Ed. Series, 1987 BTAL-330 FLUID MECHANICS Maximum Time : 3 Hrs. University Examination : 60 Marks Total Marks : 100 Continous Internal Assessment : 40 Marks Minimum Pass Marks : 40% A) Instructions for paper-setter 1. The question paper will consist five sections namely A, B, C, D and E. 2. Each of the sections A, B, C and D will contain two questions and candidates have to attempt at least one question compulsorily from each section. Each section carry 15% of the total marks 3. Section E will comprise of 10-15 short answers type questions, which will cover the entire syllabus and will carry 40% of the total marks. B) Instructions for candidates 1. Candidates are required to attempt one question each from sections A, B, C and D 2. Use of non-programmable scientific calculator is allowed. SECTION A Fluid properties, real and ideal fluid, fluid statics, buoyancy. Classification of flows:compressible and incompressible flows, steady and unsteady flows, uniform and non- uniform flows, laminar and turbulent flows. SECTION B Continuity equation, momentum equation and applications, energy equation and applications. Ideal fluid flow: irrotational flow, velocity potential, source, doublet, vortex, circulation and vorticity, flowpast circular cylinder and sphere. SECTION C Real fluid flow: Boundary layer, drag, incompressible internal and external flows. SECTION D One dimensional compressible flow; dimensional analysis and similarity. REFERENCES 1. Douglas, J.F., Gasiorek, J.M. and Swaffield, J.A., "Fluid Mechanics", Longman ELBS, 1992. 2. White F.M., Fluid Mechanics, McGraw Hill, 1979. . BTINT-340 AIRCRAFT PRODUCTION Maximum Time : 3 Hrs. University Examination : 60 Marks Total Marks : 100 Continous Internal Assessment : 40 Marks Minimum Pass Marks : 40% A) Instructions for paper-setter 1. The question paper will consist five sections namely A, B, C, D and E. 2. Each of the sections A, B, C and D will contain two questions and candidates have to attempt at least one question compulsorily from each section. Each section carry 15% of the total marks 3. Section E will comprise of 10-15 short answers type questions, which will cover the entire syllabus and will carry 40% of the total marks. B) Instructions for candidates 1. Candidates are required to attempt one question each from sections A, B, C and D of the question paper and the entire section E. 2. Use of non-programmable scientific calculator is allowed. SECTION A Introduction to metal forming,machining and joining processes. Classification of aircraft parts. Aircraft materials. Aircraft production fundamentals. SECTION B Loft-template method. Computer-aided manufacturing. Aircraft tooling concepts. Forming processes: Rubber-pad forming, Stretch-bending, stretch-wrap forming, high energy rate forming. Unconventional machining processes. SECTION C Casting processes. Manufacturing processes for typical aircraft and aeroengine parts. Adhesive bonding, riveting, detachable joints, honeycomb sandwich construction. Design and fabrication of tooling. Aircraft assembly techniques and tooling. SECTION D Heat treatment.Surface treatments, protective treatments and coatings. Fabrication, machining and joining of FRP composite structures. Characteristics of aerospace vehicle construction. REFRENCES 1. D.F. Horne, Aircraft Production Technology, Cambridge University Press, 1986. 2. S.C. Keshu and K.K. Ganapathi, Aircraft Production,Interline Publishing, 1993. 3. M.M. Schwartz (ed.),Composite Materials Handbook, McGraw-Hill, 1992. FOURTH SEMESTER BTAL-410 MEASUREMENTS AND INSTRUMENTATION Maximum Time : 3 Hrs. University Examination : 30 Marks Total Marks : 50 Continous Internal Assessment : 20 Marks Minimum Pass Marks: 40% A) Instructions for paper-setter 1. The question paper will consist five sections namely A, B, C, D and E. 2. Each of the sections A, B, C and D will contain two questions and candidates have to attempt at least one question compulsorily from each section. Each section carry 15% of the total marks 3. Section E will comprise of 10-15 short answers type questions, which will cover the entire syllabus and will carry 40% of the total marks. B) Instructions for candidates 1. Candidates are required to attempt one question each from sections A, B, C and D of the question paper and the entire section E. 2. Use of non-programmable scientific calculator is allowed. SECTION A Elements of Measuring Systems and their functions, Calibration, Validity of results, Standards of Measurements, Accuracy, Precision, Sensitivity, Linearity, Hysteresis, Loading Effects, Resolution etc. SECTION B Order of the sensor/instrument, Time constant, Rise time, Settling time, Dead time, Frequency & Damping. Error analysis motion, strain/force, fluid flow, pressure, flow velocity and direction, temperature and heat flux, sound pressure, frequency and phase. SECTION C Fundamentals of Electronics, semiconductor transistors & diodes, small signal circuit analysis & gain relations, operational amplifier, instrumentation amplifier, filters, modulators and demodulators. SECTION D Fundamentals of digital circuits, logic gates, A/D and D/A converters, multiplexers, microprocessor etc. REFERENCES 1. E.Doeblin, Measurement Systems: Application and Design, 4th Edition, McGraw-Hill, New York, 1990. 2. R.G. Beckwith, N.L. Buck & R.D. Marangoni, Mechanical Measurements, 3rd Edition, Narosa Pub. House, New Delhi, 1989. 3. B.C. Nakra & K.K. Chaudhary, Instrumentation Measurement & Analysis, Tata McGraw- Hill, New Delhi, 1985. J.Millman & C.C. Halkias, Integrated Electronics, Tata McGraw-Hill, New Delhi, 1992. ]BTAL-410 P MEASUREMENTS AND INSTRUMENTATION Maximum Time : 3 Hrs. University Examination : 60 Marks Total Marks : 100 Continous Internal Assessment : 40 Marks Minimum Pass Marks : 40% Experiments on analogue devices such as diodes, transistors, operational amplifiers. Digital circuit introduction using flip-flops, gates and microprocessor. Experiments in aerodynamics, propulsion and structures labs.for familiarization with engineering measurements. BTINT-420 AEROSPACE STRUCTURES I Maximum Time : 3 Hrs. University Examination : 60 Marks Total Marks : 100 Continous Internal Assessment : 40 Marks Minimum Pass Marks : 40% A) Instructions for paper-setter 1. The question paper will consist five sections namely A, B, C, D and E. 2. Each of the sections A, B, C and D will contain two questions and candidates have to attempt at least one question compulsorily from each section. Each section carry 15% of the total marks 3. Section E will comprise of 10-15 short answers type questions, which will cover the entire syllabus and will carry 40% of the total marks. B) Instructions for candidates 1. Candidates are required to attempt one question each from sections A, B, C and D of the question paper and the entire section E. 2. Use of non-programmable scientific calculator is allowed. SECTION A Introduction to Matter-Environment and Interactions. Concepts of Force fields, Equilibrium and Compatibility, techniques and practices for writing internal force diagrams (AFD/TD/SFD& BMD). SECTION B Theory of deformation of ID continuum subjected to axial,torsional, bending and buckling loads. SECTION C States of stress/strain at a point. Principle stresses and strains. Stress/strain transformations and Mohrs circle. SECTION D Failure mechanisms,design of one-dimensional structures and joints. REFERENCES 1. Gere J.M. and Timoshenko, S.P., Mechanics of Materials, CBS Publishers, 1986. 2. Byars E.F., Snyder R.D. and Plants H.L., Engineering Mechanics of Deformable Bodies, 4th Ed., Harper and Row Publishers, 1983. 3. S.P. Timoshenko and J.N. Goodier, Theory of Elasticity, 3rd ed. McGraw Hill Book Co., 1982. BTAL-430 TURBOMACHINES Maximum Time : 3 Hrs. University Examination : 60 Marks Total Marks : 100 Continous Internal Assessment : 40 Marks Minimum Pass Marks : 40% A) Instructions for paper-setter 1. The question paper will consist five sections namely A, B, C, D and E. 2. Each of the sections A, B, C and D will contain two questions and candidates have to attempt at least one question compulsorily from each section. Each section carry 15% of the total marks 3. Section E will comprise of 10-15 short answers type questions, which will cover the entire syllabus and will carry 40% of the total marks. B) Instructions for candidates 1. Candidates are required to attempt one question each from sections A, B, C and D of the question paper and the entire section E. 2. Use of non-programmable scientific calculator is allowed. SECTION A Introduction to Turbomachines: Air/Gas flow machines, Turbochargers,Pumps, Blowers, Fans, Gas/Steam Turbines, Wind Turbines. Theories of Turbomachinery; Relevant Aero- Thermodynamic laws; Equations of fluid motion; velocity diagrams; Losses; Choking and Cavitation; Blade/Vane Loading; SECTION B Design considerations for compressors, fans, blowers & pumps, wind turbines, steam/gas turbines, hydraulic turbines. SECTION C Application/Installation specific designs. Modeling of Turbomachnery flows; Dynamic similarity in turbomachinery performance rating; Performance maps. SECTION D Experimental development; standards, Instrumentation, Calibration and uncertainty of testing; Design/Test/Installed performance of turbomachines REFERENCES 1. Earl Logan (Jr.), Turbomachinery : Basic Theory and Applications, Marcel Dekkar, 1993. 2. David Japikse and N.C. Baines, Introduction to Turbomachinery concepts, Oxford, 1994. BTAL-440 AEROSPACE STRUCTURES II Maximum Time : 3 Hrs. University Examination : 60 Marks Total Marks : 100 Continous Internal Assessment : 40 Marks Minimum Pass Marks: 40% A) Instructions for paper-setter 1. The question paper will consist five sections namely A, B, C, D and E. 2. Each of the sections A, B, C and D will contain two questions and candidates have to attempt at least one question compulsorily from each section. Each section carry 15% of the total marks 3. Section E will comprise of 10-15 short answers type questions, which will cover the entire syllabus and will carry 40% of the total marks. B) Instructions for candidates 1. Candidates are required to attempt one question each from sections A, B, C and D of the question paper and the entire section E. 2. Use of non-programmable scientific calculator is allowed. SECTION A Introduction to 3-D elasticity and Airy"s stress function. St.Venants Theory of Torsion. Energy theorems and their applications. SECTION B Rayleigh methods of structural analysis with continuum and discrete coordinates. SECTION C Concepts and principles of structural analysis and modelling. Development of simplified structural models and their applications to A/c components. SECTION D Introduction to matrix methods of structural analysis and computer aided design. REFRENCES 1. T.H.G. Megson, Aircraft Structures for Engineering Students, 2nd Edward Arnold London, 1990. 2. Irving H. Shames and Clive L. Dym., "Energy and Finite Element Methods on Structural Mechanics, Hemisphere Pub Corporation, McGraw-Hill Book Co., N.Y. 1985. 3. E.F. Bruhn, Analysis and Design of Flight Vehicle Structures, Tri-State Offset Co., Cincinnati, Ohio, USA, 1965. FIFTH SEMESTER BTAL-510 FLIGHT MECHANICS II Maximum Time : 3 Hrs. University Examination : 60 Marks Total Marks : 100 Continous Internal Assessment : 40 Marks Minimum Pass Marks : 40% A) Instructions for paper-setter 1. The question paper will consist five sections namely A, B, C, D and E. 2. Each of the sections A, B, C and D will contain two questions and candidates have to attempt at least one question compulsorily from each section. Each section carry 15% of the total marks 3. Section E will comprise of 10-15 short answers type questions, which will cover the entire syllabus and will carry 40% of the total marks. B) Instructions for candidates 1. Candidates are required to attempt one question each from sections A, B, C and D of the question paper and the entire section E. 2. Use of non-programmable scientific calculator is allowed. SECTION A Static stability; longitudinal neutral point in stick fixed and stick free conditions, directional stability; Longitudinal & directional control. SECTION B Lateral stability and control. Equations of motion of rigid aircraft in body fixed axes. Stability axes, stability derivatives. SECTION C Steady flight and perturbed flight. Various longitudinal and lateral-directional modes. Linearisation of the equations of motion. SECTION D Decoupling of lateral-directional motion from longitudinal motion. REFERENCES 1. J. Roskam, Flight Mechanics of Rigid and Elastic Airplanes, University of Kansas Press, 1972. 2. R.C.Nelson, Flight Stability & Automatic Control, Mc Graw Hiil International, 1990. 3. Perkins, C.D. and Hage, R.E., Airplane Performance Stability and Control, Wiley, New York, 1949. BTAL-520 SYSTEM MODELLING AND DYNAMICS Maximum Time : 3 Hrs. University Examination : 60 Marks Total Marks : 100 Continuous Internal Assessment : 40 Marks Minimum Pass Marks: 40% A) Instructions for paper-setter 1. The question paper will consist five sections namely A, B, C, D and E. 2. Each of the sections A, B, C and D will contain two questions and candidates have to attempt at least one question compulsorily from each section. Each section carry 15% of the total marks 3. Section E will comprise of 10-15 short answers type questions, which will cover the entire syllabus and will carry 40% of the total marks. B) Instructions for candidates 1. Candidates are required to attempt one question each from sections A, B, C and D of the question paper and the entire section E. 2. Use of non-programmable scientific calculator is allowed. SECTION A Introduction to modelling of systems: objective, concepts, types of models, Examples of interacting dynamic systems. Dynamic classical models of smple physical systems: Fluid level, Thermal, Electrical and Mechanical networks. SECTION B Dynamic Models of Electrical and Hydraulic actuation systems, typical complex systems. Block Diagram representation and manipulation. Signal flow graph, Masons Gain formula. Laplace Transform, Transfer function, Transient response of First and second order systems. Characteristic Equation, representation on "s" plane. SECTION C Concept of stability, Rouths criterion. Introduction to state space Models and Eigenvalues. Single degree of freedom system vibrations, Free and Forced Undamped and Damped SECTION D Vibrations, Introduction to Vibration Isolation. REFERENCES 1. K. Ogata, "Modern Control Engineering", Prentice-Hall India,New Delhi,1986. 2. J.J.D"Azzo & C.H. Houpis, "Linear Control System Analysis and Design", 4th Ed., McGraw Hill, New York, 1995. 3. W. Weaver, S.P. Timoshenko and D.H. Young, "Vibration Problems in Engineering", 5th ed., John-Wiley & Sons, 1990. BTAL-530 CONTROL THEORY Maximum Time : 3 Hrs. University Examination : 60 Marks Total Marks : 100 Continous Internal Assessment : 40 Marks Minimum Pass Marks: 40% A) Instructions for paper-setter 1. The question paper will consist five sections namely A, B, C, D and E. 2. Each of the sections A, B, C and D will contain two questions and candidates have to attempt at least one question compulsorily from each section. Each section carry 15% of the total marks 3. Section E will comprise of 10-15 short answers type questions, which will cover the entire syllabus and will carry 40% of the total marks. B) Instructions for candidates 1. Candidates are required to attempt one question each from sections A, B, C and D of the question paper and the entire section E. 2. Use of non-programmable scientific calculator is allowed. SECTION A Feedback control : mechanism of feedback, system representation, open and closed loop systems , Introduction to laplace transform, laplace transform of system, equations and concept of s- plane representation of system characteristic equation, routh s stability criterion. SECTION B Transient response and steady state error analysis : Frequency domain : root locus plots, frequency response, nyquist plots and Bode diagrams, robustness and stability margins , compensation via lead. SECTION C Lag and lead-lag compensators, stability margins. Introduction to optimum control concepts such as performance index etc. SECTION D Introduction to digital control system and z- transform techniques. REFERENCES 1. K.Ogata, "Modern Control Engineering", Prentice Hall India, 1986. 2. F.H.Raven, "Automatic Control Engineering", Fourth Edition, McGraw-Hill Book Co., 1987. 3. B.C.Kuo, "Automatic Control Systems", Fifth Edition, Prentice Hall India, 1990 BTAL-540 AIRCRAFT PROPULSION Maximum Time : 3 Hrs. University Examination : 60 Marks Total Marks : 100 Continous Internal Assessment : 40 Marks Minimum Pass Marks : 40% A) Instructions for paper-setter 1. The question paper will consist five sections namely A, B, C, D and E. 2. Each of the sections A, B, C and D will contain two questions and candidates have to attempt at least one question compulsorily from each section. Each section carry 15% of the total marks 3. Section E will comprise of 10-15 short answers type questions, which will cover the entire syllabus and will carry 40% of the total marks. B) Instructions for candidates 1. Candidates are required to attempt one question each from sections A, B, C and D of the question paper and the entire section E. 2 Use of non-programmable scientific calculator is allowed SECTION A Introduction to various aircraft propulsive devices: Piston-prop, Turboprop, Turbojet, Turbofan, Turboshaft, Ramjet, Vectored-thrust, Lift engines. SECTION B Gas Turbine cycles and cycle based performance analysis; 1-D and 2-D analysis of flow through gas turbine components -Intake, Compressors, Turbines, Combustion Chamber, Afterburner, and nozzle. SECTION C Compressor and Turbine blade shapes; cascade theory; radial equilibrium theory; matching of compressor and turbine. Turbine cooling. SECTION D Single spool Multi-spool engines. Powerplant performance with varying speed and altitude. REFERENCES 1. Cohen, Rogers and Saravanamutto, Gas Turbine Theory Longman,1987. 2. G.C Oates (Ed.) Aerothermodynamics of Aircraft Engine Components,AIAA, 1985. SIXTH SEMESTER BTAL-610 P AERODYNAMICS LABORATORY Maximum Time : 3 Hrs. University Examination : 60 Marks Total Marks :100 Continous Internal Assessment : 40 Marks Minimum Pass Marks : 40% The laboratory course will comprise of exercises on what is learnt in the theory classes of the same course i.e. FLUID MECHANICS I-II. BTAL-620 AEROSPACE STRUCTURES III Maximum Time : 3 Hrs. University Examination : 60 Marks Total Marks : 100 Continous Internal Assessment : 40 Marks Minimum Pass Marks : 40% A) Instructions for paper-setter 1. The question paper will consist five sections namely A, B, C, D and E. 2. Each of the sections A, B, C and D will contain two questions and candidates have to attempt at least one question compulsorily from each section. Each section carry 15% of the total marks 3. Section E will comprise of 10-15 short answers type questions, which will cover the entire syllabus and will carry 40% of the total marks. B) Instructions for candidates 1. Candidates are required to attempt one question each from sections A, B, C and D of the question paper and the entire section E. 2. Use of non-programmable scientific calculator is allowed. SECTION A Thin-walled stiffened structures in aerospace vehicles, basic components and assemblages. General formulation for thin-walled beams. SECTION B Bending and torsion of thin-walled beams of arbitrary closed and open cross-sections, shear flow and shear centre calculations for general cross-sections,warpless cross-sections. Bending and torsion of multi-cell thin-walled beams - warping, shear flow and shear centre, stresses in thin-walled beams of variable depth, effect of taper. SECTION C Effect of warp restraint in thin-walled beams, axial constraint stresses, effect of warp restraint in open section beams. Buckling of thin walled beams, torsional instability, introduction to the instability of flat sheets, local buckling of composite shapes, buckling of stiffened sheets, effective width concept, design charts and formulae. SECTION D Diagonal tension and semi-tension field beams. REFRENCES 1. T.H.G.Megson, Aircraft Structures for Engineering Students, 2nd ed. Edward Arnold, London, 1990. 2. E.F.Bruhn, Analysis and Design of Flight Vehicle Structures, Tri-State Offset Co.,Cincinnati, Ohio, U.S.A. 1965 3. D.Williams, Introduction to the Theory of Aircraft Structures, Edward Arnold, London, 1960. BTAL-630 AERODYNAMICS OF AEROSPACE VEHICLES Maximum Time : 3 Hrs. University Examination : 60 Marks Total Marks : 100 Continous Internal Assessment : 40 Marks Minimum Pass Marks: 40% A) Instructions for paper-setter 1. The question paper will consist five sections namely A, B, C, D and E. 2. Each of the sections A, B, C and D will contain two questions and candidates have to attempt at least one question compulsorily from each section. Each section carry 15% of the total marks 3. Section E will comprise of 10-15 short answers type questions, which will cover the entire syllabus and will carry 40% of the total marks. B) Instructions for candidates 1. Candidates are required to attempt one question each from sections A, B, C and D of the question paper and the entire section E. 2. Use of non-programmable scientific calculator is allowed. SECTION A Potential flow, Circulation and lift generation, Kutta cndition. Thin airfoil theory, Source, Vortex and doublet panel methods. SECTION B Subsonic compressible flow over airfoils, Prandtl-Glauert Compressibility correction. Supersonic flow over airfoils, Ackeret Theory. Oblique shocks and expansion waves, shock expansion method. SECTION C Potential flow over finite wings, lifting-line theory, Vortex lattice method, supersonc flow over finite wings, Subsonic/supersonic leading edge. Linearized theory, Supersonic vortex lattice method. Slender body theory. SECTION D Introduction to transonic flows, conical flows, Hypersonic flow and high-temperature flows. REFERENCES 1. J.D. Anderson, Fundamentals of Aerodynamics, McGraw Hill, 1991 2. J.J.Bertin & M.C. Smith, Aerodynamics for Engineers, 1989 3. A.M. Kuethe & C.Chow, Foundations of Aerodynamics, J. Wiley, 1986 4. H.Ashly & M.T. Landahl, Aerodynamics of Wings & Bodies, Addison Wesley, 1965. . BTAL-640 P AIRCRAFT STRUCTURES LABORATORY Maximum Time : 3 Hrs. University Examination : 60 Marks Total Marks : 100 Continous Internal Assessment : 40 Marks Minimum Pass Marks: 40% Experiments on composite laminate fabrication, determination of Poissons ratio, determination of shear centre, tension and flexure testing, compression and impact testing, interlaminar shear, study of UTMs coefficient of thermal expansion, determination of young"s modulus by vibration,determination of natural frequencies, and damping modal analysis by impact excitation, drop-weight impact test. SEVENTH SEMESTER BTAL-710 MECHANISMS & MACHINE DESIGN Maximum Time : 3 Hrs. University Examination : 60 Marks Total Marks : 100 Continous Internal Assessment : 40 Marks Minimum Pass Marks: 40% A) Instructions for paper-setter 1. The question paper will consist five sections namely A, B, C, D and E. 2. Each of the sections A, B, C and D will contain two questions and candidates have to attempt at least one question compulsorily from each section. Each section carry 15% of the total marks 3. Section E will comprise of 10-15 short answers type questions, which will cover the entire syllabus and will carry 40% of the total marks. B) Instructions for candidates 1. Candidates are required to attempt one question each from sections A, B, C and D of the question paper and the entire section E. 2. Use of non-programmable scientific calculator is allowed. SECTION A Elements of kinematics and dynamics of mechanisms; Motion and force analysis of typical mechanisms, e.g. link mechanisms, universal joint, cams, gears. SECTION B General principles of Mechanical Design: Dimensioning, limits of fits and tolerances; Failure and mechanical properties of materials, Concepts in allowable stresses, reliability and lifing. SECTION C Design analysis of common machine elements, e.g. joints, springs, shafts, couplings etc. SECTION D Terminology and classification concerning gears, bearings, seals. Concepts in lubrication. REFERENCES 1. T. Bevan, Theory of Machines, Longmans, 1956. 2. J.E. Shigley, Mechanical Engineering Design, Mc-Graw Hill Book Co., 1986. BTAL-720 COMPUTATIONAL FLUID DYNAMICS Maximum Time : 3 Hrs. University Examination : 60 Marks Total Marks : 100 Continous Internal Assessment : 40 MarksMinimum Pass Marks: 40% A) Instructions for paper-setter 1. The question paper will consist five sections namely A, B, C, D and E. 2. Each of the sections A, B, C and D will contain two questions and candidates have to attempt at least one question compulsorily from each section. Each section carry 15% of the total marks 3. Section E will comprise of 10-15 short answers type questions, which will cover the entire syllabus and will carry 40% of the total marks. B) Instructions for candidates 1. Candidates are required to attempt one question each from sections A, B, C and D of the question paper and the entire section E. 2. Use of non-programmable scientific calculator is allowed. SECTION A Basic equations of fluid dynamics and levels of approximation. Mathematical nature of the flow equations and their boundary conditions. SECTION B Grid and appropriate transformation. Basic discretization techniques applied to model equations and system of equations: finite difference, finite volume and finite element methods. SECTION C Analysis of numerical schemes : concept consistency, stability and convergence. Error and stability analysis. SECTION D Some applications. REFERENCES 1. Hirsch C., Numerical Computation of Internal and External Flows, John Wiley and Sons, 1990. 2. Anderson J.D., Computational Fluid Dynamics, 1995. 3. Anderson D.A., Tenehill J.C. & Pletcher R.H., Computational Fluid Dynamics and Heat Transfer, McGraw Hill, 1984. BTAL-730 AIRCRAFT DESIGN Maximum Time : 3 Hrs. University Examination : 60 Marks Total Marks : 100 Continous Internal Assessment : 40 Marks Minimum Pass Marks : 40% A) Instructions for paper-setter 1. The question paper will consist five sections namely A, B, C, D and E. 2. Each of the sections A, B, C and D will contain two questions and candidates have to attempt at least one question compulsorily from each section. Each section carry 15% of the total marks 3. Section E will comprise of 10-15 short answers type questions, which will cover the entire syllabus and will carry 40% of the total marks. B) Instructions for candidates 1. Candidates are required to attempt one question each from sections A, B, C and D of the question paper and the entire section E. 2. Use of non-programmable scientific calculator is allowed. SECTION A Types of Aerial vehicles, their basic principles,advantages/disadvantages/limitations. Product/system design process Formulation of problem-objective function, constraints. Solutions. SECTION B Aircraft project phases. Configuration: Types and comparison of wing, Tail, Fuselage, Landing Gear, Wing-Tail combinations, Powerplant (types, numbers, locations). Estimation of C, Field length, Allowable CG range, Thrust vs. speed & altitude for propeller and jet. SECTION C Estimation of preliminary weight, Acquisition cost. Operating cost. Rubber Engine Sizing: Fixed engine sizing. Detailed weights, detailed geometry etc. SECTION D Detailed design: V-n diagram, design loads, structural layout. Introduction to advanced concepts in aircraft design REFRENCES 1. Daniel P.Raymer, Aircraft Design - A Conceptual Approach, AIAA Educational Series, 1990. 2. E.Torenbeek, Synthesis of Subsonic Airplane Design, Delft University Press, 1977. BTAL-740 CONTROL SYSTEMS LABORATORY Maximum Time : 3 Hrs. University Examination : 60 Marks Total Marks : 100 Continous Internal Assessment : 40 Marks Minimum Pass Marks : 40% Experiments using typical analogue and digital control system setups. Frequency Response tests and other related control theory concept validation with physical systems, Analog simulation of simple systems & Aircraft Longitudinal Dynamics. BTAL-810 SPACEFLIGHT MECHANICS Maximum Time : 3 Hrs. University Examination : 60 Marks Total Marks : 100 Continous Internal Assessment : 40 Marks Minimum Pass Marks: 40% A) Instructions for paper-setter 1. The question paper will consist five sections namely A, B, C, D and E. 2. Each of the sections A, B, C and D will contain two questions and candidates have to attempt at least one question compulsorily from each section. Each section carry 15% of the total marks 3. Section E will comprise of 10-15 short answers type questions, which will cover the entire syllabus and will carry 40% of the total marks. B) Instructions for candidates 1. Candidates are required to attempt one question each from sections A, B, C and D of the question paper and the entire section E. 2. Use of non-programmable scientific calculator is allowed. SECTION A Introduction to spacecrafts, rockets and missiles, their basic functions and features, some examples. Fundamentals of Rocket Performance, simplified equations of variable mass rocket motion. SECTION B Evaluation of rocket/missile trajectories as projectile motion, rectilinear motion in vacuum & in atmosphere, velocity-mass relations and other performance calculations and the gravity turn trajectory. SECTION C Jet damping effect and concept of multistaging in launch vehicles and missiles. Fundamentals of constrained optimization in multistage rockets. Central force motion, Two body and three body problem, Keppler"s laws of planetary motion, Geometry of conic sections and orbit determination from initial conditions. SECTION D Spacecraft orbit transfer, attitude motion, stability and control of the attitude motion REFERENCES 1. M.H. Kaplan, Modern Spacecraft Dynamics and control, John Wiley & Sons, London, 1976. 2. J.W.Cornelisse, Rocket Propulsion and Spaceflight Dynamics, Pitman, London, 1979 3. W.T. Thompson,Introduction to Space Dynamics, John Wiley & Sons, London, 1963. BTAL-820 INTRODUCTION TO COMPOSITE STRUCTURES Maximum Time : 3 Hrs. University Examination : 60 Marks Total Marks : 100 Continous Internal Assessment : 40 Marks Minimum Pass Marks : 40% A) Instructions for paper-setter 1. The question paper will consist five sections namely A, B, C, D and E. 2. Each of the sections A, B, C and D will contain two questions and candidates have to attempt at least one question compulsorily from each section. Each section carry 15% of the total marks 3. Section E will comprise of 10-15 short answers type questions, which will cover the entire syllabus and will carry 40% of the total marks. B) Instructions for candidates 1. Candidates are required to attempt one question each from sections A, B, C and D of the question paper and the entire section E. 2. Use of non-programmable scientific calculator is allowed. SECTION A Fiber reinforced Composites in aerospace structures. Fibers and polymeric matrix materials. Fabrication processes. Introduction to anisotropic elasticity, Unidirectional composites, Micromechanics,Interfaces and interphases in polymer composites. SECTION B Lamination theory and free edge effects. Stress and failure analysis of laminated composites. SECTION C Hygrothermal and environmental effects. Testing of composite materials. Some design concepts for polymer matrix composite structures. SECTION D Intelligent composites, design approach. REFRENCES 1. R.M. Jones, Mechanics of composite Materials, Taylor & Francis, 1999. 2. D. Hull and T.W. Clyne, An Introduction to Composite Materials, Cambridge University Press, 1996. 3. L.N. Phillips (ed.), Design with Advanced Composite Materials, Springer-Verlag, 1989. BTAL-830 EL(1) DYNAMICAL SYSTEMS Maximum Time : 3 Hrs. University Examination : 60 Marks Total Marks : 100 Continous Internal Assessment : 40 Marks Minimum Pass Marks : 40% A) Instructions for paper-setter 1. The question paper will consist five sections namely A, B, C, D and E. 2. Each of the sections A, B, C and D will contain two questions and candidates have to attempt at least one question compulsorily from each section. Each section carry 15% of the total marks 3. Section E will comprise of 10-15 short answers type questions, which will cover the entire syllabus and will carry 40% of the total marks. B) Instructions for candidates 1. Candidates are required to attempt one question each from sections A, B, C and D of the question paper and the entire section E. 2.Use of non-programmable scientific calculator is allowed. SECTION A Kenneth H. Huebner, The Finite Element Method for Engineers, John Wiley and Sons, Mathematical Modeling; DT Non-linear systems . SECTION B Local theory - equilibrium points, stability, linear systems, controllability, perturbation methods; Linear time-variant systems, linear periodic systems. SECTION C State-space analysis; Non-linear stability - time-domain and frequency domain. SECTION D Introduction to bifurcation and chaos. REFRENCES 1. Mohler R.R., Nonlinear systems, Vol.I - Dynamics and Control, Prentice Hall, 1991 2. Verhulst, F., Nonlinear Differential Equations and Dynamical Systems, Springer-Verlag, 1990 3. Hirsch, M.W. and Smale, S., Differential Equations, Dynamical Systems and Linear Algebra, Academic Press, 1974. 4. Wiggins, S., Introduction to Applied Nonlinear Dynamical Systems and Chaos, Springer- Verlag, 1990. BTAL-840 EL(2) GAS DYNAMICS Maximum Time : 3 Hrs. University Examination : 60 Marks Total Marks : 100 Continous Internal Assessment : 40 Marks Minimum Pass Marks : 40% A) Instructions for paper-setter 1. The question paper will consist five sections namely A, B, C, D and E. 2. Each of the sections A, B, C and D will contain two questions and candidates have to attempt at least one question compulsorily from each section. Each section carry 15% of the total marks 3. Section E will comprise of 10-15 short answers type questions, which will cover the entire syllabus and will carry 40% of the total marks. B) Instructions for candidates 1. Candidates are required to attempt one question each from sections A, B, C and D of the question paper and the entire section E. 2. Use of non-programmable scientific calculator is allowed. SECTION A Fundamentals of thermodynamics; propagation of small disturbances in gases; nozzle flow; SECTION B One-dimensional unsteady flow; small disturbance theory of supersonic speeds SECTION C supersonic flow over two-dimensional bodies. SECTION D Shock expansion analysis, method of characteristics; one-dimensional rarefaction and compression waves flow in a shock tube. REFRENCES 1.Liepmann H W and Roshko A, Elements of Gas Dynamics, John Wiley,1957 2.Owczarek J A Fundamentals of Gas Dynamics, International Test Books Co.,1968 3.Becker E, Gas Dynamics Academic Press, New York, 1968. BTAL-840 PROJECT Maximum Time :3 Hrs. University Examination : 60 Marks Total Marks :100 Continuous Internal Assessment : 40 Marks Minimum Pass Marks :40% 1. Students are supposed to spend 45-55 hours on the project. The internal teacher must monitor progress of the project. Students can arrange the project at their own level, however, Institute can also assist in getting the project and can issue necessary letters etc. 2. The external examiner will distribute marks allocated for University examination for viva/project report and for other activity, which the external examiner thinks to be proper. Maximum Marks for the project 60% Max marks for viva 40% 3. Joint projects will be allowed and joint project reports will also be accepted. The students should highlight their contributions in a joint project report. 4. the students have to submit two copies of project. The examiners will evaluate these reports on the spot at the time of examination and will conduct the viva.