Integral Equation Method for Subsonic Flow Past Airfoils in Ventilated Wind Tunnels
- 1 January 1975
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 13 (1) , 47-53
- https://doi.org/10.2514/3.49629
Abstract
No abstract availableKeywords
This publication has 5 references indexed in Scilit:
- Wind-Tunnel Wall Interference Reduction by Streamwise Porosity DistributionAIAA Journal, 1972
- Calculation of potential flow about arbitrary bodiesProgress in Aerospace Sciences, 1967
- Transonic wind tunnel test sectionsZeitschrift für angewandte Mathematik und Physik, 1956
- Compressibility Effects in AerodynamicsJournal of the Aeronautical Sciences, 1941
- The effect of compressibility on the lift of an aerofoilProceedings of the Royal Society of London. Series A, Containing Papers of a Mathematical and Physical Character, 1928