The Instability of Pitching Oscillations of an Airfoil in Subsonic Incompressible Potential Flow-Reference-Cited by-同舟云学术

The Instability of Pitching Oscillations of an Airfoil in Subsonic Incompressible Potential Flow

Published:1949-11 Issue:11 Volume:16 Page:691-696
ISSN:1936-9956
Container-title:Journal of the Aeronautical Sciences
language:en
Short-container-title:Journal of the Aeronautical Sciences

Author:

SMILG BENJAMIN¹

Affiliation:

1. Wright-Patterson Air Force Base,

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Link

http://arc.aiaa.org/doi/pdf/10.2514/8.11885

Reference4 articles.

1. Smilg, B., The Prevention of Aileron Oscillations at Transonic Airspeeds, Air Force Technical Report 5530,December, 1946.

2. Cheilik, H., and Frissel, H., Theoretical Criteria for Single Degree of Freedom Flutter at Supersonic Speeds, Cornell Aeronautical Laboratory Report CAL-7A, May, 1947.

3. Smilg, B., and Wasserman, L. S., Application of Three-Dimensional Flutter Theory to Aircraft Structures, Air Force Technical Report 4798,July, 1942.

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