Flight, Wind Tunnel, and Numerical Experiments with a Slender Cone at Incidence

This publication has 6 references indexed in Scilit:

• Flight experiments with a slender cone at angle of attack
  Published by American Institute of Aeronautics and Astronautics (AIAA) ,1981
• A computational and experimental study of high Reynolds number viscous/inviscid interaction about a cone at high angle of attack
  Published by American Institute of Aeronautics and Astronautics (AIAA) ,1980
• Control of forebody vortex orientation to alleviate side forces
  Published by American Institute of Aeronautics and Astronautics (AIAA) ,1980
• Boundary-layer transition on a 10-deg cone - Wind tunnel/flight correlation
  Published by American Institute of Aeronautics and Astronautics (AIAA) ,1980
• Numerical Simulation of Shock Wave - Turbulent Boundary-Layer Interaction
  AIAA Journal, 1976
• Flow separation about elliptic cones at incidence
  Published by American Institute of Aeronautics and Astronautics (AIAA) ,1965