Near wake uniqueness and a re-examination of the throat concept in laminar mixing theory
- 23 January 1967
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 10 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
- A study of laminar near wakes.AIAA Journal, 1966
- An experimental investigation of the near wake of a slender cone at M infinity equal 8 and 12.AIAA Journal, 1966
- Near wake flow field measurements.AIAA Journal, 1965
- Theory of laminar near wake of blunt bodies in hypersonic flow.AIAA Journal, 1965
- I. Eigenmotion analysisProceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences, 1965
- Viscous and resistive eddies near a sharp cornerJournal of Fluid Mechanics, 1964
- On steady laminar flow with closed streamlines at large Reynolds numberJournal of Fluid Mechanics, 1956
- A Mixing Theory for the Interaction Between Dissipative Flows and Nearly Isentropic StreamsJournal of the Aeronautical Sciences, 1952