An approximate calculation of the onset velocity of cavity oscillations

Author:

COVERT EUGENE E.1

Affiliation:

1. Massachusetts Institute of Technology, Cambridge, Mass.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference24 articles.

1. ^ The solution for G and Gc may be deduced using Refs. 9, 12 or frompp.554et seq., 728 et seq. of Morse,P. M.and Ingard, K. U., Theoretical Acoustics,McGraw Hill, New York,1968, and Ref. 14. The computation is not difficult but is lengthy. Interested readers may request from the author a copy of M.I.T. Aerophysics Report 38, as long as they are available, if they wish to see the details of the computations for G Gcand the infinite determinant.

2. Rayleigh, J. W. S., The Theory of Sound, Vol.2, Macmillan, Ltd., London,1896, pp.412-414.

3. The vortex motion causing edge tones

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