H. Harris Hamilton

• Application of a numerically generated orthogonal coordinate system to the solution of inviscid axisymmetric supersonic flow over blunt bodies
• Calculation of convective and radiative heating on the forebody heatshield of the aeroassist flight experiment vehicle
• Calculation of laminar heating rates on three-dimensional configurations using the axisymmetric analogue
• Finite-difference solution for laminar or turbulent boundary layer flow over axisymmetric bodies with ideal gas, CF,́ or equilibrium air chemistry
• Finite-difference solution for laminar or turbulent boundary layer flow over axisymmetric bodies with ideal gas, CF4, or equilibrium air chemistry
• Finite-differnce solution for laminar or turbulent boundary layer flow over axisymmetric bodies with ideal gas, CF, or equilibrium air chemistry
• Solution of axisymmetric and two-dimensional inviscid flow over blunt bodies by the method of lines
• Time-dependent solution for axisymmetric flow over a blunt body with ideal gas, CF, or equilibrium air chemistry