A Theoretical Model of the Near Wake of a Slender Body in Supersonic Flow
- 1 September 1972
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 10 (9) , 1165-1172
- https://doi.org/10.2514/3.50344
Abstract
No abstract availableThis publication has 12 references indexed in Scilit:
- On the two-dimensional viscous counterpart of the one-dimensional sonic throatJournal of Fluid Mechanics, 1969
- Upstream Influence in Viscous Interaction ProblemsPhysics of Fluids, 1968
- An interaction model of a supersonic laminar boundary layer on sharpand rounded backward facing steps.AIAA Journal, 1968
- Experimental studies on the lip shock.AIAA Journal, 1968
- A new theoretical solution of the laminar, hypersonic near wake.AIAA Journal, 1967
- Interacting supersonic laminar wake calculations by a finite difference method.AIAA Journal, 1967
- Laminar boundary-layer separation and near-wake flow for a smooth blunt body at supersonic and hypersonic speeds.AIAA Journal, 1967
- On the hypersonic laminar near wake critical point of the Crocco-Lees mixing theoryPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1967
- Theory of laminar near wake of blunt bodies in hypersonic flow.AIAA Journal, 1965
- A Mixing Theory for the Interaction Between Dissipative Flows and Nearly Isentropic StreamsJournal of the Aeronautical Sciences, 1952