Aerodynamic comparison of a conical and biconic reentry vehicle

This publication has 5 references indexed in Scilit:

• A comparison of hypersonic wind tunnel data obtained by static and free oscillation testing techniques
  Published by American Institute of Aeronautics and Astronautics (AIAA) ,1977
• Three dimensional supersonic inviscid flow field calculations on reentry vehicles with control surfaces
  Published by American Institute of Aeronautics and Astronautics (AIAA) ,1977
• Inviscid Supersonic/Hypersonic Body Flowfield and Aerodynamicsfrom Shock-Capturing Technique Calculations
  Journal of Spacecraft and Rockets, 1976
• Ablative nose shape change effects on re-entry vehicle aerodynamic performance
  Published by American Institute of Aeronautics and Astronautics (AIAA) ,1972
• Comment on the location of the center of pressure of a right circular cone using Newtonian impact theory.
  AIAA Journal, 1966