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Certificate of Registration Media number Эл #ФС77-53688 of 17 April 2013. ISSN 2308-6033. DOI 10.18698/2308-6033
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Shock-wave structures control methods in the input section of the aircraft high-speed air intake

Published: 21.02.2023

Authors: Laptinskaya M.M., Savelova K.E., Chernyshov M.V.

Published in issue: #2(134)/2023

DOI: 10.18698/2308-6033-2023-2-2249

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

    supersonic air intake, aircraft, energy supply, gas permeable surfaces, shock-wave structures, dynamic compatibility conditions, numerical simulation
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