Analysis of the near-wake pressure in supersonic flow using the momentum integral method.
- 1 October 1966
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 3 (10) , 1504-1509
- https://doi.org/10.2514/3.28685
Abstract
No abstract availableKeywords
This publication has 5 references indexed in Scilit:
- Theory of laminar near wake of blunt bodies in hypersonic flow.AIAA Journal, 1965
- Momentum integral methods for the laminar free shear layerAIAA Journal, 1964
- COMPRESSIBLE FREE SHEAR LAYER WITH FINITE INITIAL THICKNESSAIAA Journal, 1963
- Theory for Supersonic, Two-Dimensional, Laminar, Base-Type Flows Using the Crocco-Lees Mixing ConceptsJournal of the Aerospace Sciences, 1962
- A Mixing Theory for the Interaction Between Dissipative Flows and Nearly Isentropic StreamsJournal of the Aeronautical Sciences, 1952