A study of the laminar near-wake behind a cylinder at Mach 20.
- 1 July 1966
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 4 (7), 1187-1194
- https://doi.org/10.2514/3.3647
Abstract
No abstract availableThis publication has 14 references indexed in Scilit:
- Theory of laminar near wake of blunt bodies in hypersonic flow.AIAA Journal, 1965
- Near wake of a blunt body at hypersonic speedsAIAA Journal, 1965
- Turbulent diffusion of a reacting wakeAIAA Journal, 1965
- Finite-difference calculation of hypersonic wakesAIAA Journal, 1964
- Hypersonic laminar wakes and transition studiesAIAA Journal, 1964
- A study of wakes behind a circular cylinder at m equal 5.7AIAA Journal, 1964
- Momentum integral methods for the laminar free shear layerAIAA Journal, 1964
- NONEQUILIBRIUM WAKES WITH LAMINAR AND TURBULENT TRANSPORTPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1963
- COMPRESSIBLE FREE SHEAR LAYER WITH FINITE INITIAL THICKNESSAIAA Journal, 1963
- Turbulent Diffusion in the Wake of a Blunt-Nosed Body at Hypersonic SpeedsJournal of the Aerospace Sciences, 1962