Prediction of Unsteady Airloads for Oblique Blade-Gust Interaction in Compressible Flow
- 1 September 1974
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 12 (9) , 1228-1235
- https://doi.org/10.2514/3.49458
Abstract
No abstract availableKeywords
This publication has 6 references indexed in Scilit:
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- Some Aspects of Non-Stationary Airfoil Theory and Its Practical ApplicationJournal of the Aeronautical Sciences, 1941