Normal injection in a three-dimensional laminar boundary layer.
- 1 February 1969
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 7 (2) , 367-369
- https://doi.org/10.2514/3.5111
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- An investigation of the reflected shock interaction process in a shock tube.AIAA Journal, 1968
- A high density, high velocity equilibrium freestream shock tunnel conceptPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1968
- Comment on "Nonequilibrium Effects on High-Enthalpy Expansion of Air"AIAA Journal, 1966
- Shock tube test time limitation due to turbulentwall boundary layerAIAA Journal, 1964