Numerical investigation  of the transonic flow around the above-caliber head part model of the carrier rocket taking into account acoustic disturbances in the flow

Borisov V. E.; Kudryashov I.Y.; Lutsky A. E.

Abstract:

The preprint is devoted to the study of a number of problems associated with transonic flow problems. The solution structure evolution is determined in the range of Mach numbers 1.038 - 1.095 with a the uniform incoming flow. The influence of incident flow disturbances on the flow parameters at M = 1.038 has been investigated.

Keywords:

transonic flow, separation region, closing jump, acoustic disturbances

Publication language: russian, pages: 16

Research direction:

Mathematical modelling in actual problems of science and technics

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About authors:

Borisov Vitaly Evgenyevich, , ,

Kudryashov Ivan Yurievich, , ,

Lutsky Alexander Evgenievich, , ,