Computation of three-dimensional viscous flow over blunt lifting bodies at high angle of attack
- 23 June 1981
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Three-dimensional hypersonic laminar, transitional and/or turbulent shock-layer flowsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1980
- Viscous flow over arbitrary geometries at high angle of attackPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1980
- Numerical solution of the hypersonic viscous shock-layer equationsAIAA Journal, 1970