Oblique Compressible Sears Function
Author:
Affiliation:
1. Ministry of Transport, Ottawa, Canada
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.49556
Reference11 articles.
1. Some Aspects of Non-Stationary Airfoil Theory and Its Practical Application
2. Unsteady thin-airfoil theory for subsonic flow.
3. Prediction of Unsteady Airloads for Oblique Blade-Gust Interaction in Compressible Flow
4. Similarity rules for thin aerofoils in non-stationary subsonic flows
5. A lifting-surface solution for vortex-induced airloads
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3. Subsonic unsteady aerodynamics caused by gusts using the indicial method;Journal of Aircraft;1996-09
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