Shape effects on hypersonic slender body wake geometry and transition distance.
- 1 May 1967
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 4 (5) , 657-662
- https://doi.org/10.2514/3.28924
Abstract
No abstract availableKeywords
This publication has 7 references indexed in Scilit:
- Transition and Strouhal Number for the Incompressible Wake of Various BodiesPhysics of Fluids, 1966
- Relationship of laminar wake width to wake transition distance.AIAA Journal, 1965
- Hypersonic laminar wakes and transition studiesAIAA Journal, 1964
- A study of wakes behind a circular cylinder at m equal 5.7AIAA Journal, 1964
- Transition correlations for hypersonic wakesAIAA Journal, 1964
- Hot-wire measurements in the hypersonic wakes of slender bodiesAIAA Journal, 1964
- Implicit Navier-Stokes solver for three-dimensional compressible flowsAIAA Journal, 1963