Influence of Wing, Fuselage, and Tail Design on Rotational Flow Aerodynamics Beyond Maximum Lift

Author:

Bihrle William1,Bowman James S.2

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

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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