Oscillating Airfoils at High Mach Number-Reference-Cited by-同舟云学术

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Oscillating Airfoils at High Mach Number

Published:1953-06 Issue:6 Volume:20 Page:402-406
ISSN:1936-9956
Container-title:Journal of the Aeronautical Sciences
language:en
Short-container-title:Journal of the Aeronautical Sciences

Author:

LIGHTHILL M. J.¹

Affiliation:

1. University of Manchester, England

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Link

http://arc.aiaa.org/doi/pdf/10.2514/8.2657

Reference4 articles.

1. Hayes, W. D., Q. App. Math., Vol. 5, pp. 105-106, 1947.

2. Goldsworthy, F. A., Q.J.M.A.M., Vol. 5, pp. 54-63, 1952.

3. Jones, W. P., The Influence of Thickness-Chord Ratio on Supersonic Derivatives for Oscillating Aerofoils, A.R.C. Report 10871 (limited circulation), to be published as A.R.C. R. & M. 2679.

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