Abstract
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.
Publisher
Cambridge University Press (CUP)
Reference3 articles.
1. The Shock Pattern of a Wing-Body Combination, Far from the Flight Path
2. 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.
3. Jones L. B. (1960). Optimisation of the Sonic Bang. English Electric Aviation Ltd. Aero. Tech. Memo. AM.28, October 1960.
Cited by
58 articles.
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