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Shock Waves from Supersonic Transports

Published online by Cambridge University Press:  07 June 2016

A. R. Seebass
A. R. Seebass*
Affiliation:
Boeing Scientific Research Laboratories
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Abstract

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Type
Correspondence
Information
Aeronautical Quarterly , Volume 21 , Issue 4 , November 1970 , pp. 408
Copyright
Copyright © Royal Aeronautical Society. 1970

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References

1. McLean, F. E. Some nonasymptotic effects on the sonic boom of large airplanes. NASA TN D-2877, June 1965.Google Scholar
2. Hayes, W. D. Brief review of the basic theory. Sonic Boom Research, NASA SP-147, p. 3, April 1967.Google Scholar
3. Seebass, R. Minimum sonic boom shock strengths and overpressures. Nature, Vol. 221, p. 651, February 1969.CrossRefGoogle ScholarPubMed
4. Seebass, R. Sonic boom theory. Journal of Aircraft, Vol. 6, p. 177, May-June 1969.Google Scholar
5. George, A. R. Lower bounds for sonic booms in the midfield. AIAA Journal Vol. 7, p. 1543, August 1969.CrossRefGoogle Scholar