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This article is cited in 1 scientific paper (total 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.
Citation:
V. E. Borisov, I. Yu. Kudryashov, A. E. Lutsky, “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”, Keldysh Institute preprints, 2018, 264, 16 pp.
Linking options:
https://www.mathnet.ru/eng/ipmp2621 https://www.mathnet.ru/eng/ipmp/y2018/p264
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