Influence of Wing, Fuselage, and Tail Design on Rotational Flow Aerodynamics Beyond Maximum Lift
Author:
Affiliation:
1. Bihrle Applied Research, Inc., Jericho, N. Y.
2. NASA Langley Research Center, Hampton, Va.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.57581
Reference16 articles.
1. 2Bamber, M.J. and Zimmerman, C.H. "The Aerodynamic Forces and Moments Exerted on a Spinning Model of the 'NY-1' Airplane as Measured by the Spinning Balance," NACA Report 456, 1933.
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