Computations of the pitching oscillation of a NACA 64A-010 airfoil in the small disturbance limit
Author:
Affiliation:
1. Boeing Military Airplane Co., Seattle, Wash.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1980-128
Reference6 articles.
1. Yoshihara, H. "Fixes to the 30 Transonic Small Disturbance Theory". Convair Report CASD-ERR-75-012, 1975.
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