Aerodynamic theory for wing with side edge passing subsonically through a gust
- 1 June 1983
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 21 (6) , 808-815
- https://doi.org/10.2514/3.8157
Abstract
No abstract availableKeywords
This publication has 5 references indexed in Scilit:
- Unified aerodynamic-acoustic theory for a thin rectangular wing encountering a gustAIAA Journal, 1980
- High frequency thin-airfoil theory for subsonic flowAIAA Journal, 1976
- Lifting-Surface Theory for a Semi-Infinite Wing in Oblique GustAIAA Journal, 1974
- Analytic Approximation Techniques in Applied MathematicsJournal of the Society for Industrial and Applied Mathematics, 1965
- Die Beugung und Polarisation des Lichts durch einen Spalt. IMathematische Annalen, 1901