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Lower Bounds for Sonic Bangs

Published online by Cambridge University Press:  04 July 2016

L. B. Jones
L. B. Jones*
Affiliation:
English Electric A viation Ltd.
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Extract

Lower bounds for the intensity of the sonic bang of a slender aircraft configuration with various constraints are given in this note which is a condensed version of Ref. 1. Although these lower bounds cannot be achieved in practice the method of obtaining them demonstrates how low values can be obtained. Special emphasis is given to a possible supersonic transport.

Type
Technical Notes
Information
The Aeronautical Journal , Volume 65 , Issue 606 , June 1961 , pp. 433 - 436
Copyright
Copyright © Royal Aeronautical Society 1961

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References

1.Jones, L. B. (1960). Optimisation of the Sonic Bang. English Electric Aviation Ltd. Aero. Tech. Memo. AM.28, October 1960.Google Scholar
2.Walkden, F. (1958). The Shock Pattern of a Wing Body Combination, far from the Flight Path. The Aeronautical Quarterly, Vol. IX, p. 164, May 1958.Google Scholar
3.Lilley, G. M. and Spillman, J. J. (1960). Ground Level Disturbance from Large Aircraft at Supersonic Speeds. College of Aeronautics, Note No. 103, May 1960.Google Scholar