Engineering Journal: Science and InnovationELECTRONIC SCIENCE AND ENGINEERING PUBLICATION
Certificate of Registration Media number Эл #ФС77-53688 of 17 April 2013. ISSN 2308-6033. DOI 10.18698/2308-6033
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Article

Flow around hypersonic aircraft models and simple geometries in a hypersonic shock tunnel

Published: 13.09.2016

Authors: Kotov M.A., Kryukov I.A., Ruleva L.B., Solodovnikov S.I., Surzhikov S.T.

Published in issue: #9(57)/2016

DOI: 10.18698/2308-6033-2016-9-1537

Category: Aviation and Rocket-Space Engineering | Chapter: Aerodynamics and Heat Transfer Processes in Aircrafts

We studied shockwave configurations obtained during hypersonic gas flow around fragments of hypersonic aircraft. The article describes our test installation. We analyse the experimental data on flows around an acute wedge and a cylinder. These models pose as "simple geometry" models for testing new computation codes. We supply the results of comparing data obtained during computation and experimentation.


References
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