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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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Aerodynamic characteristics of perforated aircraft flight controls at subsonic flow velocities

Published: 15.08.2022

Authors: Kalugin V.T., Lutsenko A.Yu., Kalugina M.D., Nazarova D.K., Slobodyanyuk D.M.

Published in issue: #8(128)/2022

DOI: 10.18698/2308-6033-2022-8-2205

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

    flight controls, aerodynamic characteristics, perforated surface, subsonic flow, wind tunnel
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