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Anna High Speed Aerodynamics Sem-V
No Units Titles Sub Titles Chapters
1 Unit 1 Fundamental aspects of compressible flow Compressibility, Continuity, Momentum and Energy equations for steady one dimensional flow, compressible Bernoulli's equation, Area - Mach number - Velocity relation, Mach cone, Mach angle, One dimensional Isentropic flow through variable area duct, Critical conditions, Characteristic Mach number, Area-Mach number relation, Maximum discharge velocity - operating characteristics of nozzles- Introduction to hypersonic flowss method VIEW CHAPTERS
2 Unit 2 Shock and expansion waves Normal shock relations, Prandtl's relation, Hugoniot equation, Rayleigh Supersonic Pitot tube equation, Moving normal shock waves, Oblique shocks, a-b-M relation, Shock Polar, Reflection of oblique shocks, left running and right running waves, Interaction of oblique shock waves, slip line, shock-boundary layer interaction - transonic lambda shock - compression corner effect - incident shock interaction - Rayleigh flow, Fanno flow, Expansion waves, Prandtl-Meyer expansion, Maximum turning angle, Simple and non-simple regions VIEW CHAPTERS
3 Unit 3 Two dimensional compressible flow Potential equation for 2-dimensional compressible flow, Linearisation of potential equation, perturbation potential, Linearised Pressure Coefficient, Linearised subsonic flow, Prandtl- Glauert rule, Linearised supersonic flow, Method of characteristics VIEW CHAPTERS
4 Unit 4 High speed flow over airfoils, wings and airplane configuration Critical Mach number, Drag divergence Mach number, Shock Stall, Supercritical Airfoil Sections, Transonic area rule, Swept wing, Airfoils for supersonic flows, Lift, drag, Pitching moment and Centre of pressure for supersonic profiles, Shock-expansion theory, wave drag, supersonic wings, Design considerations for supersonic aircraft- aerodynamic heating VIEW CHAPTERS
5 Unit 5 Experimental techniques for highspeed flows Wind tunnels for transonic, Supersonic and hypersonic flows, shock tube, Gun tunnels-peculiar problems in the operation of hypersonic tunnels - Supersonic flow visualization methods VIEW CHAPTERS
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