Airfoil trailing edge flow measurements and comparison with theory, incorporating open wind tunnel corrections
- 17 August 1984
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- Wind Tunnel Wall Corrections Deduced by Iterating from Measured Wall Static PressureAIAA Journal, 1983
- Calculation of two-dimensional near and far wakesAIAA Journal, 1982