ACOUSTIC FIELD OF THIN BODY IN A FLOW OF NONEQUILIBRIUM FLUCTUATING GAS

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Abstract

The equations describing the structure of the average acoustic field of well streamlined thin body in supersonic gas flow of the non-equilibrium random media are received. It is founded the dependence between shock wave front shape and relation of correlation radius and wave length. The results are compared with experimental data.

 

About the authors

Igor P. Zavershinskii

Samara State Aerospace University
34, Moskovskoye shosse, Samara,
443086, Russia.

Author for correspondence.
Email: ipzav63@mail.ru
Russian Federation

Vladislav N. Knestyapin

Samara State Aerospace University
34, Moskovskoye shosse, Samara,
443086, Russia.

Email: ipzav63@mail.ru
Russian Federation

Efim Ya. Коgan

Самарский государственный аэрокосмический университет имени академика С.П. Королева (национальный исследовательский университет) (СГАУ).
г. Самара, Московское шоссе, 34., 443086, Россия

Email: ipzav63@mail.ru

Samara State Aerospace University
34, Moskovskoye shosse, Samara,
443086, Russia.

Russian Federation

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