UNDERGRADUATE HIGH SPEED AERODYNAMICS
1. Review
2-D Airfoil Theory Thin Airfoil theory Panel method Panel Code Panel Code sample Input
2. Compressible potential flow equation
3. Small-disturbance form of potential equation
Linearized Potential Equation
Linearized Pressure Coefficient
Boundary Conditions
Subsonic Similarity 2-D
Airfoils in Supersonic Flow
4. Nonlinear techniques for supersonic flows
Shock-expansion technique
Busemann 2nd-order theory
Sources of drag
Drag coefficient
5. Method of characteristics for supersonic flow
2-D Nozzle design code: nozdes3.m Prandtl-Meyer find nu given Mach number
Prandtl-Meyer find Mach number given nu
6.
Wings and Bodies in Compressible Flow
Wings
in subsonic flow
Bodies
of revolution in subsonic flow
Bodies of
revolution in supersonic flow
Airfoils in Transonic Flow
Supercritical airfoils
Transonic Drag Rise
Variation of Lift with M
Sweep
Supersonic and Subsonic Leading Edges
Transonic Area Rule
8.
Introduction to
Hypersonic flow
9. Review of boundary layer theory (Derviation of Equations) BL Properties BL Summary
10. Methods for predicting laminar boundary layer effects Thwaites’ Method Application to a Cylinder
11. Transition to turbulence; physics of turbulence Transition Models Head’s Method
12. Reynolds averaging and models for turbulent stresses
13. Compressibility Effects and High Speed Aerodynamic heating Effects