Supercritical airfoil boundary-layer and near-wake measurements
- 1 April 1983
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 20 (4), 298-305
- https://doi.org/10.2514/3.44867
Abstract
No abstract availableKeywords
This publication has 5 references indexed in Scilit:
- Experiments on the Flow about a Supercritical Airfoil Including Holographic InterferometryJournal of Aircraft, 1981
- Pseudo-Direct Solution to the Boundary-Layer Equations for Separated FlowAIAA Journal, 1980
- Transonic Flow Past a Symmetrical Airfoil-Inviscid and Turbulent Flow PropertiesAIAA Journal, 1980
- Theory of viscous transonic flow over airfoils at high Reynolds numberPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1977
- Computation of Separated Transonic Turbulent FlowsAIAA Journal, 1976