Airfoil response to an incompressible skewed gust of small spanwise wave-number
- 1 April 1976
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 14 (4), 541-542
- https://doi.org/10.2514/3.7126
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Approximate unsteady thin-airfoil theory for subsonic flowAIAA Journal, 1976
- Passage of a Swept Airfoil through an Oblique GustJournal of Aircraft, 1974
- Compressibility Effects in Unsteady Thin-Airfoil TheoryAIAA Journal, 1974
- Gust Loading on a Thin AerofoilAeronautical Quarterly, 1971
- Similarity rules for thin aerofoils in non-stationary subsonic flowsJournal of Fluid Mechanics, 1970
- Lifting Surface Theory for the Problem of an Arbitrarily Yawed Sinusoidal Gust Incident on a Thin Aerofoil in Incompressible FlowAeronautical Quarterly, 1970