Viscous flow over arbitrary geometries at high angle of attack
- 14 January 1980
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 7 references indexed in Scilit:
- Computation of supersonic viscous flows over ogive-cylinders at angle of attackPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979
- Numerical simulation of steady supersonic viscousPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979
- Hypersonic viscous flows over sphere-cones at high angles of attackPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978
- Calculation of the laminar viscous shock layer on a blunt biconic body at incidence to supersonic and hypersonic flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1977
- An implicit method for three dimensional viscous flow with application to cones at angle of attackComputers & Fluids, 1975
- Calculation of the flow on a blunted cone at high angle of attackPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975
- Calculation of the Flow on a Cone at High Angle of AttackAIAA Journal, 1974