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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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The Effect of Through-Hole Perforation of the Control Surfaces on the Aerodynamic Characteristics of a Supersonic Vehicle

Published: 01.07.2026

Authors: Kalugina M.D., Lutsenko A.Yu., Popov I.O.

Published in issue: #7(175)/2026

DOI:

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

    through-perforation, flight control shields, aerodynamic characteristics, flow separation zone, numerical simulation
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