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JOURNALS // Preprints of the Keldysh Institute of Applied Mathematics // Archive

Keldysh Institute preprints, 2018 264, 16 pp. (Mi ipmp2621)

This article is cited in 1 paper

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

V. E. Borisov, I. Yu. Kudryashov, A. E. Lutsky


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.

DOI: 10.20948/prepr-2018-264



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© Steklov Math. Inst. of RAS, 2024