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For detailed syllabus of all the other subjects of Aerospace Engg 6th Sem, 2021 curriculum do visit Aerospace Engg 6th Sem subject syllabuses for 2021 regulation. For Aerospace Engineering 6th Sem semesters scheme and subjects, refer to Aerospace Engg 6th Sem 2021 regulation scheme. The scheme details of Professional Elective-VII for Aerospace Engg 6th Sem is as follows.

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For Aerospace Engineering 6th Sem scheme and its subjects, do visit Aerospace Engg 6th Sem 2021 regulation scheme. For Professional Elective-VII scheme and its subjects refer to Aerospace Engg Professional Elective-VII syllabus scheme. The detailed syllabus of missile guidance and control is as follows.

Course Objectives:

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Unit I

INTRODUCTION TO MISSILE SYSTEMS
History of guided missile for defence applications- Classification of missiles- Generalized Missile Equations of Motion- Coordinate Systems- Lagrange’s Equations for Rotating Coordinate Systems-Rigid-Body Equations of Motion-missile system elements, missile ground systems.

Unit II

MISSILE AIRFRAMES, AUTOPILOTS AND CONTROL
Missile aerodynamics- Force Equations, Moment Equations, Phases of missile flight. Missile control configurations. Missile Mathematical Model. Autopilots — Definitions, Types of Autopilots, Example Applications. Open-loop autopilots. Inertial instruments and feedback. Autopilot response, stability, and agility- Pitch Autopilot Design, Pitch-Yaw-Roll Autopilot Design.

Unit III

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Unit IV

STRATEGIC MISSILES
Introduction, Two-Body Problem, Lambert’s Theorem, First-Order Motion of a Ballistic Missile, Correlated Velocity and Velocity-to-Be-Gained Concepts, Derivation of the Force Equation for Ballistic Missiles, Atmospheric Re-entry, Ballistic Missile Intercept, Missile Tracking Equations of Motion, Introduction to Cruise Missiles, Terrain-Contour Matching (TERCOM) Concept.

Unit V

WEAPON DELIVERY SYSTEMS
Weapon Delivery Requirements, Factors Influencing Weapon Delivery Accuracy, Unguided Weapons, Bombing Problem, Guided Weapons, Integrated Flight Control in Weapon Delivery, Missile Launch Envelope, Mathematical Considerations Pertaining to the Accuracy of Weapon Delivery Computations.

Course Outcomes:

On successful completion of this course, the student will be able to

• Explain the advanced concepts of missile guidance and control to the engineers.
• Classify the necessary mathematical knowledge that are needed in understanding the physical processes.
• Have an exposure on various topics such as missile systems, missile airframes, autopilots, guidance laws and will be able to deploy these skills effectively in the understanding of missile guidance and control
• Develop linear guidance, control, and navigation laws.
• Analyse performance of the integrated guidance and navigation controller.

Text Books:

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Reference Books:

1. Garnell, P., “Guided Weapon Control Systems”, 2nd Ed., Pergamon Press, 1980.
2. Joseph Ben Asher and Isaac Yaesh, “Advances in Missile Guidance Theory”, AIAA Education series, 1998.
3. Paul Zarchan, “Tactical and Strategic Missile Guidance”, AIAA Education series, 2007.

For detailed syllabus of all the other subjects of Aerospace Engineering 6th Sem, visit Aerospace Engg 6th Sem subject syllabuses for 2021 regulation.

For all Aerospace Engineering results, visit Anna University Aerospace Engg all semester results direct link.

For Aerospace Engineering 6th Sem scheme and its subjects, do visit Aerospace Engg 6th Sem 2021 regulation scheme. For Professional Elective-VII scheme and its subjects refer to Aerospace Engg Professional Elective-VII syllabus scheme. The detailed syllabus of advanced vehicle engineering is as follows.

Course Objectives:

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Unit I

ELECTRIC VEHICLES
EV architectures, advantages and disadvantages, Electrical and mechanical energy storage technologies, battery management. Performance of Electric Vehicles, Tractive effort and Transmission requirement, Vehicle performance, Tractive effort in normal driving.

Unit II

ELECTRIC VEHICLE MOTORS
Electric Propulsion basics, motor capacity determination, Induction motor, DC motor, Permanent Magnet Motor, Switch Reluctance Motor, Configuration, Characteristics, Performance and control of Drives.

Unit III

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Unit IV

AUTOMOTIVE NETWORKING
Bus Systems – Classification, Applications in the vehicle, Coupling of networks, networked vehicles, Buses – CAN Bus, LIN Bus, MOST Bus, Bluetooth, Flex Ray, Diagnostic Interfaces.

Unit V

ON-BOARD TESTING
Integration of Sensor Data to On-Board Control Systems (OBD), OBD requirements, certification, enforcement, systems, testing, Catalytic converter and Exhaust Gas Recirculation system monitoring, Introduction to Cyber-physical system.

Course Outcomes:

At the end of the course the students would be able to

1. Acquire an overview of electric vehicles and their importance in automotive.
2. Discuss the characteristics and the selection of traction motor.
3. Comprehend the vehicle-to-vehicle and autonomous technology.
4. Explain the networking of various modules in automotive systems, communication protocols and diagnostics of the sub systems.
5. Be familiar with on-board diagnostics systems.

Text Books:

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Reference Books:

1. Dominique Paret, Multiplexed Networks for Embedded Systems, John Wiley & Sons Ltd., 2007.
2. Hong Cheng, Autonomous Intelligent Vehicles: Theory, Algorithms & Implementation!!, Springer, 2011
3. Advanced Technology Vehicles Manufacturing (ATVM) Loan Program (Energy Science, Engineering and Technology: Congressional Policies, Practices and Procedures)by Andrew M Wright and Harrison R Scott | 5 September 2012
4. Advanced Vehicle Technology by Heinz Heisler MSc BSc FIMI MIRTE MCIT | 17 July 2002
5. Advanced Motorsport Engineering: Units for Study at Level 3by Andrew Livesey | 1 September 2011

For detailed syllabus of all the other subjects of Aerospace Engineering 6th Sem, visit Aerospace Engg 6th Sem subject syllabuses for 2021 regulation.

For all Aerospace Engineering results, visit Anna University Aerospace Engg all semester results direct link.

For Aerospace Engineering 6th Sem scheme and its subjects, do visit Aerospace Engg 6th Sem 2021 regulation scheme. For Professional Elective-VII scheme and its subjects refer to Aerospace Engg Professional Elective-VII syllabus scheme. The detailed syllabus of heat transfer is as follows.

Course Objectives:

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Unit I

INTRODUCTION
Finite Difference Method-Introduction-Taylor’s series expansion – Discretization Methods Forward, backward and central differencing scheme for first order and second order Derivatives – Types of partial differential equations-Types of errors. Solution to algebraic equation-Direct Method and Indirect Method-Types of boundary condition. FDM – FEM -FVM.

Unit II

CONDUCTIVE HEAT TRANSFER
General 3D-heat conduction equation in Cartesian, cylindrical and spherical coordinates. Computation (FDM) of One -dimensional steady state heat conduction with Heat generation-without Heat generation- 2D-heat conduction problem with different boundary conditions-Numerical treatment for extended surfaces. Numerical treatment for 3D- Heat conduction. Numerical treatment to 1D-steady heat conduction using FEM.

Unit III

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Unit IV

CONVECTIVE HEAT TRANSFER
Convection- Numerical treatment (FDM) of steady and unsteady 1 -D and 2-d heat convection-diffusion steady-unsteady problems- Computation of thermal and Velocity boundary layer flows. Upwind scheme. Stream function-vorticity approach-Creeping flow.

Unit V

RADIATIVE HEAT TRANSFER
Radiation fundamentals-Shape factor calculation-Radiosity method- Absorption Method -Montacalro method-Introduction to Finite Volume ^Method- Numerical treatment of radiation enclosures using finite Volume method. Developing a numerical code for 1D, 2D heat transfer problems.

Course Outcomes:

Upon completion of this course, Students will be able to

1. Acquire knowledge on the basic concepts on the applications of numerical methods for the heat transfer problem solutions.
2. Appreciate the role of boundary conditions in defining the complexities and the methodology for numerical solutions of heat transfer problems.
3. Use both implicit and explicit schemes for transient heat conduction problems.
4. Compute the temperature profiles in thermal boundary layer.
5. Apply finite volume methods for radiative heat transfer problems and the role of Montecarlo methods in radiative heat transfer.

Text Books:

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Reference Books:

1. NecatiOzisik, Finite Difference Method in Heat Transfer, CRC Press, 2nd edition, 2017.
2. YogeshJaluria, Kenneth E Torrence, Computational Heat transfer, CRC Press, 3rd Edition, 2017.
3. Pradip Majumdar, Computational Methods for Heat & Mass Transfer, CRC Press, 2005.

For detailed syllabus of all the other subjects of Aerospace Engineering 6th Sem, visit Aerospace Engg 6th Sem subject syllabuses for 2021 regulation.

For all Aerospace Engineering results, visit Anna University Aerospace Engg all semester results direct link.

For Aerospace Engineering 6th Sem scheme and its subjects, do visit Aerospace Engg 6th Sem 2021 regulation scheme. For Professional Elective-VII scheme and its subjects refer to Aerospace Engg Professional Elective-VII syllabus scheme. The detailed syllabus of structural dynamics is as follows.

Course Objectives:

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Unit I

FORCE DEFLECTION PROPERTIES OF STRUCTURES
Constraints and Generalized coordinates – Virtual work and generalized forces – Force – Deflection influence functions – stiffness and flexibility methods.

Unit II

PRINCIPLES OF DYNAMICS
Free and forced vibrations of systems with finite degrees of freedom – Response to periodic excitation -Impulse Response Function – Convolution Integral

Unit III

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Unit IV

ENERGY METHODS
Rayleigh’s principle – Rayleigh – Ritz method – Coupled natural modes – Effect of rotary inertia and shear on lateral vibrations of beams – Natural vibrations of plates.

Unit V

APPROXIMATE METHODS
Approximate methods of evaluating the Eigen frequencies and eigen vectors by reduced, subspace, Lanczos, Power, Matrix condensation and QR methods.

Course Outcomes:

Students will be able to

1. Determine the various options of mathematical modelling of structures
2. Evaluate the response of structures under various dynamically loaded conditions
3. Explain the natural modes of vibration of structures
4. Interpret the knowledge in numerical and approximate methods of evaluating natural modes of vibration.
5. Justify the natural frequencies and mode shapes of a multi degree of freedom system

Text Books:

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Reference Books:

1. Ramamurthi. V., “Mechanical Vibration Practice and Noise Control” Narosa Publishing House Pvt. Ltd, 2008
2. Timoshenko. S.P., and D.H. Young, “Vibration Problems in Engineering”, John Willey & SonsInc., 1984.
3. Vierck. R.K., “Vibration Analysis”, 2nd Edition, Thomas Y. Crowell & Co Harper & Row Publishers, New York, U.S.A. 1989.

For detailed syllabus of all the other subjects of Aerospace Engineering 6th Sem, visit Aerospace Engg 6th Sem subject syllabuses for 2021 regulation.

For all Aerospace Engineering results, visit Anna University Aerospace Engg all semester results direct link.

For Aerospace Engineering 6th Sem scheme and its subjects, do visit Aerospace Engg 6th Sem 2021 regulation scheme. For Professional Elective-VII scheme and its subjects refer to Aerospace Engg Professional Elective-VII syllabus scheme. The detailed syllabus of theory of elasticity is as follows.

Course Objectives:

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Unit I

BASIC EQUATIONS OF ELASTICITY
Definition of Stress and Strain: Stress – Strain relationships – Equations of Equilibrium, Compatibility equations, Boundary Conditions, Saint Venant’s principle – Principal Stresses, Stress Ellipsoid – Stress invariants.

Unit II

PLANE STRESS AND PLANE STRAIN PROBLEMS
Airy’s stress function, Bi-harmonic equations, Polynomial solutions, Simple two-dimensional problems in Cartesian coordinates like bending of cantilever and simply supported beams.

Unit III

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Unit IV

TORSION
Navier’s theory, St. Venant’s theory, Prandtl’s theory on torsion, semi- inverse method and applications to shafts of circular, elliptical, equilateral triangular and rectangular sections. Membrane Analogy.

Unit V

INTRODUCTION TO THEORY OF PLATES AND SHELLS
Classical plate theory – Assumptions – Governing equations – Boundary conditions – Navier’s method of solution for simply supported rectangular plates – Levy’s method of solution for rectangular plates under different boundary conditions.

Course Outcomes:

At the end of the course, Students will be able to

1. Estimate the linear elasticity in the analysis of structures such as beams, plates etc.
2. Determine the facture mechanics of the curved beam subject to loads.
3. Interpret the two dimensional problems in cartesian and polar coordinates
4. Determine the response of elastomers based objects
5. Explain the structural section subjected to torsion

Text Books:

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Reference Books:

1. Barber, J. R., Elasticity (Solid Mechanics and Its Applications), Springer publishers, 3rd edition, 2010.
2. Sokolnikoff, I. S., Mathematical Theory of Elasticity, McGraw – Hill, New York, 1978.
3. Volterra& J.H. Caines, Advanced Strength of Materials, Prentice Hall, New Jersey, 1991.
4. Wang, C. T., Applied Elasticity, McGraw – Hill Co., New York, 1993.

For detailed syllabus of all the other subjects of Aerospace Engineering 6th Sem, visit Aerospace Engg 6th Sem subject syllabuses for 2021 regulation.

For all Aerospace Engineering results, visit Anna University Aerospace Engg all semester results direct link.

For Aerospace Engineering 6th Sem scheme and its subjects, do visit Aerospace Engg 6th Sem 2021 regulation scheme. For Professional Elective-VII scheme and its subjects refer to Aerospace Engg Professional Elective-VII syllabus scheme. The detailed syllabus of boundary layer theory is as follows.

Course Objectives:

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Unit I

FUNDAMENTAL EQUATIONS OF VISCOUS FLOW
Fundamental equations of viscous flow, Conservation of mass, Conservation of Momentum-Navier-Stokes equations, Energy equation, Mathematical character of basic equations, Dimensional parameters in viscous flow, Non – dimensionlisation the basic equations and boundary conditions, vorticity considerations, creeping flow and boundary layer flow.

Unit II

SOLUTIONS OF VISCOUS FLOW EQUATIONS
Solutions of viscous flow equations, Couette flows, Hagen-Poisuelle flow, Flow between rotating concentric cylinders, Combined Couette-Poiseuille Flow between parallel plates, Creeping motion, Stokes solution for an immersed sphere, Development of boundary layer, Displacement thickness, momentum and energy thickness.

Unit III

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Unit IV

TURBULENT BOUNDARY LAYER
Turbulence-physical and mathematical description, Two-dimensional turbulent boundary layer equations — Velocity profiles – The law of the wall – The law of the wake – Turbulent flow in pipes and channels – Turbulent boundary layer on a flat plate – Boundary layers with pressure gradient, Eddy Viscosity and mixing length.

Unit V

BOUNDARY LAYER CONTROL
Boundary layer control in laminar flow-Methods of Boundary layer control: Acceleration of the boundary layer-Suction- Injection of a different gas-Prevention of transition – Cooling of the wall-Boundary layer suction- Practical examples of Boundary Layer Control.

Course Outcomes:

Upon completion of this course, Students will be able to

1. Apply fundamental equations of the viscous flow for practical examples.
2. Analyze the viscous flow problems for solutions.
3. Explain the importance of viscosity and shear flow adjacent to the airframe of the aerospace vehicles.
4. Build an understanding about the laminar boundary layer concepts and solution methods.
5. Illustration about the importance of turbulence boundary layer in an aerospace engineering problem.

Text Books:

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Reference Books:

1. A.J. Reynolds, “Turbulent flows in Engineering”, John Wiley & Sons, 1980.
2. Frank White – Viscous Fluid flow – McGraw Hill, 1998
3. H. Schlichting, “Boundary Layer Theory”, McGraw-Hill, New York, 1979.
4. Ronald L., Panton, “Incompressible fluid flow”, John Wiley & Sons, 1984.
5. Tuncer Cebeci and Peter Bradshaw, “Momentum transfer in boundary layers”, Hemisphere Publishing Corporation, 1977.

For detailed syllabus of all the other subjects of Aerospace Engineering 6th Sem, visit Aerospace Engg 6th Sem subject syllabuses for 2021 regulation.

For all Aerospace Engineering results, visit Anna University Aerospace Engg all semester results direct link.

Download the iStudy App for all syllabus and other updates.

For detailed syllabus of all the other subjects of Aerospace Engg 6th Sem, 2021 curriculum do visit Aerospace Engg 6th Sem subject syllabuses for 2021 regulation. For Aerospace Engineering 6th Sem semesters scheme and subjects, refer to Aerospace Engg 6th Sem 2021 regulation scheme. The scheme details of Professional Elective-VI for Aerospace Engg 6th Sem is as follows.

Don’t forget to download iStudy App for the latest syllabus, results, class timetable and many more features. In case of questions, don’t feel shy to leave a comment or leave feedback in the iStudy app for faster response.

For the results of Aerospace Engineering 6th Sem, kindly visit Aerospace Engg 6th Sem direct results link.

For exam time table of Aerospace Engineering (Aerospace Engg), kindly visit Anna University exam timetables.

For Aerospace Engineering (Aerospace Engg) notices, kindly visit Anna University notices.

Download the iStudy App for all syllabus and other updates.

For updated syllabus of Aerospace Engineering (Aerospace Engg) 2021, kindly visit Aerospace Engg updated syllabus.

Wishing you great luck ahead.

For Aerospace Engineering 6th Sem scheme and its subjects, do visit Aerospace Engg 6th Sem 2021 regulation scheme. For Professional Elective-VI scheme and its subjects refer to Aerospace Engg Professional Elective-VI syllabus scheme. The detailed syllabus of smart materials and structures is as follows.

Course Objectives:

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Unit I

OVERVIEW AND INTRODUCTION
Piezoelectric Material Crystal Structure – Fundamentals of Piezoelectricity – Shape Memory Alloys – Fundamentals of Shape Memory Alloy (SMA) Behaviour – Phase Transformation -Lattice Structure and Deformation Mechanism – Electrostrictive Material Systems – ER and MR Fluids – Current Application – Aerospace Field – Machine Tools – Automotive Systems -Medical Systems – Electronics Equipment – Robots – Energy Harvesting Using Smart Materials.

Unit II

PIEZOELECTRIC THEORY
Electromechanical Constitutive Equations – Piezo ceramic Actuator & Sensor Equations -Piezoelectric Coupling Coefficients – Actuator ^Performance and Load Line Analysis -Hysteresis and Nonlinearities in Piezoelectric Materials – Piezo ceramic Actuators – Behavior under Static & Dynamic Excitation Fields – Depoling Behavior and Dielectric Breakdown -Curie Temperature – Power Consumption – Equivalent Circuits to Model Piezo ceramic Actuators – The Bimorph Sensor.

Unit III

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Unit IV

UNDERSTANDING SHAPE MEMORY ALLOYS (SMA)
Low Temperature Stress-Strain Curve – Origin of the One-Way Shape Memory Effect – Stress Induced Martensite and Pseudoelasticity – Two-Way Shape Memory Effect – All-Round Shape Memory Effect – R-Phase Transformation – Porous SMA – Constrained Behavior of SMA -Free Recovery – Constrained Recovery – Effective Load-Lines of an SMA Wire Actuator -Sample Preparation – Transformation Temperatures under Zero Stress.

Unit V

CONSTITUTIVE MODELLING AND SMA BEHAVIOUR
Tanaka Model – Liang and Rogers Model – Brinson Model – Testing of SMA Wires -Variation of Transformation Temperatures with Stress – Stress-Strain Behavior at Constant Temperature – Stress-Temperature Behavior at Constant Strain – Heat Absorbed by the SMA Wire – Thermomechanical Energy EquilibriumPower Requirements for SMA Activation -Resistance Behavior of SMA Wires – Heat Dissipation – SMA Wire Damping Capacity.

Course Outcomes:

Upon completion of this course, Students will be able to

1. Classify the various forms of functional materials.
2. Investigate the Piezoelectric material behaviour.
3. Investigate the behaviour of SMA material.
4. Model a beam with Piezoelectric patch.
5. Impart knowledge on modelling of SMA material.

Text Books:

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Reference Books:

1. Martin, J.W., Engineering Materials, Their properties and Applications, Wykedham Publications (London) Ltd., 1987.
2. Prasad, N. Eswara, Wanhill, R. J. H, ‘Aerospace Materials and Material Technologies – Indian Institute of Metals Series, 2017.
3. Sam Zhang, ‘Aerospace Materials Handbook (Advances in Materials Science and Engineering) 1st Edition , 2016.
4. Van Vlack.L.H., Elements of Materials Science and Engineering Prentice Hall; Publishers, Sixth edition, 1989.

For detailed syllabus of all the other subjects of Aerospace Engineering 6th Sem, visit Aerospace Engg 6th Sem subject syllabuses for 2021 regulation.

For all Aerospace Engineering results, visit Anna University Aerospace Engg all semester results direct link.

For Aerospace Engineering 6th Sem scheme and its subjects, do visit Aerospace Engg 6th Sem 2021 regulation scheme. For Professional Elective-VI scheme and its subjects refer to Aerospace Engg Professional Elective-VI syllabus scheme. The detailed syllabus of spacecraft structures is as follows.

Course Objectives:

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Unit I

SPACECRAFT DESIGN LOADS
Transportation load factors – Steady-State Loads – Mechanical Dynamic loads – Acoustic loads -Shock loads – Static pressure variations – Micro-meteorites / Orbital Debris.

Unit II

DESIGN OF SPACECRAFT STRUCTURE
Introduction – Determination of Spacecraft Configuration – First Design Spacecraft Structure -Basic Design Supporting Structure – Detailed Analyses – Manufacturing of the spacecraft structure.

Unit III

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Unit IV

FATIGUE LIFE PREDICTION
Introduction – Palmgren-Miner Linear Cumulative Damage Rule – Analysis of Load-time Histories – Failure due to Sinusoidal Vibrations – Failure due to Narrow-banded Random Vibrations.

Unit V

DAMAGE TO SPACECRAFT BY METEOROIDS AND ORBITAL DEBRIS9
Introduction – Micro-Meteoroids and Space Debris Environment – Micro-Meteoroids Environment – Orbital debris Environment – Hyper Velocity Impact Damage Models – Single Plate Penetration Equations – Multi-shock shield – Probability of Impacts.

Course Outcomes:

On successful completion of this course, the student will be able to

• Identify simplifying assumptions and applicability of 1 structural element theories.
• Solve by hand simple 1-D axial deformation, torsion, and bending problems.
• Solve more complex structural mechanics problems using commercial finite element software.
• Solve simple discrete degree of freedom structural stability problems.
• Solve simple structural dynamics problems.

Text Books:

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Reference Books:

1. Carl C. Osgood, “Spacecraft Structures”, Prentice-Hall, 1966.
2. Junqiao Xiong, “Spacecraft Structures, Materials and Mechanical Testing”, Trans Tech Publication, 2013.

For detailed syllabus of all the other subjects of Aerospace Engineering 6th Sem, visit Aerospace Engg 6th Sem subject syllabuses for 2021 regulation.

For all Aerospace Engineering results, visit Anna University Aerospace Engg all semester results direct link.