Further results of viscous interaction theory for the laminar supersonic near wake
- 23 January 1967
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Interacting supersonic laminar wake calculations by a finite difference methodPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1966
- Theory of laminar near wake of blunt bodies in hypersonic flow.AIAA Journal, 1965
- Further solutions of the Falkner-Skan equationMathematical Proceedings of the Cambridge Philosophical Society, 1954