Viscous Flow over Arbitrary Geometries at High Angle of Attack

This publication has 6 references indexed in Scilit:

• Computation of supersonic viscous flows over ogive-cylinders at angle of attack
  Published by American Institute of Aeronautics and Astronautics (AIAA) ,1979
• Calculation of supersonic viscous flow over delta wings with sharp subsonic leading edges
  Published by American Institute of Aeronautics and Astronautics (AIAA) ,1978
• Computation of hypersonic laminar viscous flow past spinning sharp and blunt cones at high angle of attack
  Published by American Institute of Aeronautics and Astronautics (AIAA) ,1978
• An implicit method for three dimensional viscous flow with application to cones at angle of attack
  Computers & Fluids, 1975
• Calculation of the flow on a blunted cone at high angle of attack
  Published by American Institute of Aeronautics and Astronautics (AIAA) ,1975
• Calculation of the Flow on a Cone at High Angle of Attack
  AIAA Journal, 1974