Lifting-Surface Theory for a Semi-Infinite Wing in Oblique Gust
- 1 December 1974
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 12 (12) , 1672-1678
- https://doi.org/10.2514/3.49577
Abstract
No abstract availableThis publication has 7 references indexed in Scilit:
- Prediction of Unsteady Airloads for Oblique Blade-Gust Interaction in Compressible FlowAIAA Journal, 1974
- A lifting-surface solution for vortex-induced airloadsAIAA Journal, 1971
- The aerodynamic noise of small-perturbation subsonic flowsJournal of Fluid Mechanics, 1970
- 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
- Numerical lifting-surface theory - Problems and progress.AIAA Journal, 1968
- Unsteady Air Loads on Helicopter Rotor BladesJournal of the Royal Aeronautical Society, 1964