Hypersonic Laminar Viscous Flow Past Spinning Cones at Angle of Attack

This publication has 13 references indexed in Scilit:

• Computational meshes for boundary layer problems
  Published by Springer Nature ,2008
• Viscous flow over arbitrary geometries at high angle of attack
  Published by American Institute of Aeronautics and Astronautics (AIAA) ,1980
• Computation of three-dimensional viscous supersonic flow in inlets
  Published by American Institute of Aeronautics and Astronautics (AIAA) ,1980
• 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
• Magnus forces on spinning supersonic cones. II - Inviscid flow
  AIAA Journal, 1976
• Magnus Forces on Spinning Supersonic Cones -Part I: The Boundary Layer
  AIAA Journal, 1976
• An implicit method for three dimensional viscous flow with application to cones at angle of attack
  Computers & Fluids, 1975
• Viscous Flow over Spinning Cones at Angle of Attack
  AIAA Journal, 1974
• Calculation of the flow on a cone at high angle of attack
  Published by American Institute of Aeronautics and Astronautics (AIAA) ,1973