Disadvantages of thin airfoil formulations for closely coupled airfoils
- 1 June 1983
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 20 (6) , 574-576
- https://doi.org/10.2514/3.44912
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Wall curvature and transition effects in turbulent boundary layersAIAA Journal, 1971
- Das Problem des senkrechten Stoßes an einer gekrümmten WandZAMM - Journal of Applied Mathematics and Mechanics / Zeitschrift für Angewandte Mathematik und Mechanik, 1960
- On boundary layers and upstream influence II. Supersonic flows without separationProceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences, 1953