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Determination of the optimal system of shock waves in the air intake taking into account the dissociation of the incoming air molecules
| Authors: Bugay V.V., Shostov A.K. | Published: 15.02.2023 |
| Published in issue: #1(78)/2023 | |
| DOI: DOI: 10.18698/2541-8009-2023-1-857 | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
| Keywords: mach number, shock wave, air intake, supersonic flow, mathematical modeling, maximum total pressure, dissociation of molecules, deceleration parameters | |