# High Speed Aero Dynamics

IIT Kharagpur, , Prof. K.P. Sinhamahapatra

Updated On 02 Feb, 19

IIT Kharagpur, , Prof. K.P. Sinhamahapatra

Updated On 02 Feb, 19

Contents:

Basic concepts of compressible flow - continuity, energy and momentum equations; One-dimensional inviscid flow; Stagnation quantities; Isentropic conditions; Speed of sound and Mach number; Isentropic relations; Area-velocity relation - Flow through constant area duct; Normal shock; Propagating Normal Shock - One-dimensional linear and nonlinear wave motion; Linear and Nonlinear Shock tube

Oblique shock and supersonic compression by turning; Weak shocks and Mach waves; Supersonic expansion by turning; Prandtl-Meyer expansion fan; Reflection and intersection of shocks; Shock detachment and bow shock; Shock-Expansion theory with application to thin airfoils - Flow through converging and converging-diverging ducts; Flow through constant area duct with friction (Fanno flow) and - Flow through constant area duct with hear addition (Rayleigh flow) - Relation between vorticity and entropy Croccos equation; Compressible potential flow; Potential and Stream functions;

Linearized subsonic and supersonic flow theory; Small Perturbation Equation Subsonic, Supersonic and Transonic flows; Ackerets problem; Supersonic thin airfoil theory - Slender body theory; Singularity solutions; Affine transformation - Method of characteristics; Compatibility equations and method of solutions for isentropic and non-isentropic flows; Method of finite waves - Similarity rules for subsonic, supersonic and transonic flows; Critical Mach number of an airfoil

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4.1 ( 11 )

High Speed Aero Dynamics by Dr. K.P. Sinhamahapatra, Department of Aerospace Engineering, IITKharagpur. For more details on NPTEL visit httpnptel.iitm.ac.in

Sam

Sep 12, 2018

Excellent course helped me understand topic that i couldn't while attendinfg my college.

Dembe

March 29, 2019

Great course. Thank you very much.