A new facility and technique for two-dimensional aerodynamic testing
- 1 June 1983
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 20 (6), 543-551
- https://doi.org/10.2514/3.44906
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- The effects of sidewall boundary layers in two-dimensional subsonic and transonic wind tunnelsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1981
- Computation of Separated Transonic Turbulent FlowsAIAA Journal, 1976
- Transonic Flow about a Thick Circular-Arc AirfoilAIAA Journal, 1976
- Numerical Simulation of High Reynolds Number Transonic FlowsAIAA Journal, 1975