Subsonic/Supersonic Yawed Gust over an Airfoil
Author:
Affiliation:
1. Instituto Tecnologico de Aeronautica, Sao Jose dos Campos, 12228-900 SP, Brazil
2. Empresa Brasileira de Aeronautica S.A., Sao Jose dos Campos, 12227-901 SP, Brazil
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.107
Reference16 articles.
1. Lifting Surface Theory for the Problem of an Arbitrarily Yawed Sinusoidal Gust Incident on a Thin Aerofoil in Incompressible Flow
2. Similarity rules for thin aerofoils in non-stationary subsonic flows
3. Aerodynamic response of airfoils in sinusoidal oblique gust
4. Unsteady thin-airfoil theory for subsonic flow.
5. Compressibility Effects in Unsteady Thin-Airfoil Theory
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1. Prediction of fan broadband noise;4th AIAA/CEAS Aeroacoustics Conference;1998-06-02
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