Hello sir I wabt to do B.Engg in aerospace engg from IISC bou I don’t have detail knowledge of it can you please give me the syllabus of it ?

[Vishal Kotkar]

Here I am providing the detailed syllabus for B.E (Aerospace Engg) program of IISC Bangalore.

Flight and Space Mechanics:
Pioneers in aerospace history; basics of flight; airflow in standard atmosphere; airplane aerodynamics-airfoils and finite drag surfaces; thrust, power, level flight, gliding, take-off, landing and basic maneuvers; airplane performance, stability and control; mechanics of launch vehicles and satellites; introduction to aerospace design, structural components and engine options; glimpses of new technologies like unmanned, micro aerial and hypersonic vehicles.

Flight Vehicle Structures:
Characteristics of aircraft structures and materials. Introduction to elasticity. Torsion. Bending and flexural shear. Flexural shear flow in thin-walled sections. Elastic buckling. Failure theories. Variational principles and energy methods. Analysis of composite laminates. Loads on aircraft. Basic aeroelasticity

Engineering Optimization:
Applied aspects of static, deterministic and smooth optimization in engineering design and manufacturing. Topics include formulation of engineering optimization problems, optimization methods applied to unconstrained and constrained linear and nonlinear functions of one or more variables, solution evaluation and sensitivity analysis, and practicalities in engineering optimization modeling and methods. Introduction to response surface methods and genetic algorithms. Note: This course is now offered as part of the Indo-French Cyber University with Professor M. Masmoudi, University of Toulouse, via the IISc digital library.

Introduction to Helicopters:
Hovering axial flight and autorotation, Rigid blade flapping in forward flight, Multiblade coordinates, Different reference planes, Helicopter quasi-steady and unsteady aerodynamics, Rotor wake modeling and dynamic stall. Floquet theory, Introduction to rotor control performance and vibration. Helicopter design process.

Rotary Wing Aeroelasticity:
Rotational dynamics and gyroscopics: simplified gyroscope equation, precessional characteristics of rotors. Dynamics of rotating beams: hinged rigid blades, the Euler and Timoshenko beam and basic differential equation for transverse bending, rotor speed characteristics and fan plots, out-of-plane vs. inplane bending. Fuselage vibrations: forced response and vibrations, the rotor as an excitation source and filter, rotor-fuselage interaction, 1P vibrations. Linear stability analysis methods: constant coefficients, Floquet theory. Blade aeromechanical instabilities: air mass dynamics, quasi-static aerodynamics, flap-lag instability. Linear unsteady aerodynamics: general frequency domain theories, finite state formulations. Bending-torsion flutter: basic flutter theory, general analysis methods, bending-torsion of rotor blades. Nonlinear aeroelastic stability analyses: nonlinear unsteady aerodynamics, stall flutter, subharmonic responses. Rotor-fuselage coupled instabilities: propeller-nacelle whirl flutter, ground resonance, air resonance.