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Звуковой удар

34223

Чернышев С.Л.

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The monograph outlines the theoretical foundations of sonic boom, methods for its calculation and minimization. The results of systematic studies on the influence of the layout of an aircraft, its flight mode and the state of an inhomogeneous atmosphere on the sonic boom are presented, including estimates of the influence of atmospheric turbulence, dispersion and absorption on the dynamics of shock wave attenuation. Considerable attention is paid to the estimates of the minimum possible levels of sonic boom for given values of the weight of the aircraft and its main geometrical parameters. Practical recommendations are given for the formation of aircraft layouts with a low level of sonic boom. Examples of supersonic aircraft configurations with a low level of sonic boom are given.

Data sheet

ISBN 978-5-02-037961-9
Publisher Наука. Москва. 2011
Bookbinding твердый переплет, 350 стр. иллюстрации, библиография.

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ISIA Media Verlag UG (L)

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Germany
03416870612

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