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Journal of the Aeronautical Sciences (Institute of the Aeronautical Sciences)
Article . 1953 . Peer-reviewed
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Oscillating Airfoils at High Mach Number

Oscillating airfoils at high Mach number
descriptionPublicationkeyboard_double_arrow_right Article 01 Jun 1953 English Publisher:American Institute of Aeronautics and Astronautics (AIAA)Journal:Journal of the Aeronautical Sciences, volume 20, pages 402-406 (eissn: 1936-9956, Copyright policy )
Authors: M. J. Lighthill;

doi: 10.2514/8.2657

Oscillating Airfoils at High Mach Number

Abstract

A simple formula is given for the pressure distribution on an oscillating airfoil in two-dimensional flow at high Mach Number. The formula is expected to be reasonably accurate if the pressure on the surface remains within the range 0.2 to 3.5 times the mainstream pressure. To illustrate the application of the formula, some results for symmetrical airfoils performing pitching oscillations are obtained and compared with results obtained from existing theories in the case of high Mach Number.

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fluid mechanics

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citations
This is an alternative to the "Influence" indicator, which also reflects the overall/total impact of an article in the research community at large, based on the underlying citation network (diachronically).
BIP!Citations provided by BIP!
popularity
This indicator reflects the "current" impact/attention (the "hype") of an article in the research community at large, based on the underlying citation network.
BIP!Popularity provided by BIP!
influence
This indicator reflects the overall/total impact of an article in the research community at large, based on the underlying citation network (diachronically).
BIP!Influence provided by BIP!
impulse
This indicator reflects the initial momentum of an article directly after its publication, based on the underlying citation network.
BIP!Impulse provided by BIP!
262
Top 1%
Top 0.1%
Top 10%
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