Interacting supersonic laminar wake calculations by a finite difference method.
- 1 July 1967
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 5 (7) , 1224-1230
- https://doi.org/10.2514/3.4175
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Base pressure of slender bodies in laminar, hypersonic flow.AIAA Journal, 1966
- Hypersonic boundary-layer separation and the base flow problem.AIAA Journal, 1966
- Theory of laminar near wake of blunt bodies in hypersonic flow.AIAA Journal, 1965
- Wake-like solutions of the laminar boundary- layer equationsAIAA Journal, 1964
- Supersonic separated and reattaching laminar flows- i - general theory and application to adiabatic boundary layer-shock wave interactionsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1964
- A Mixing Theory for the Interaction Between Dissipative Flows and Nearly Isentropic StreamsJournal of the Aeronautical Sciences, 1952