This paper contains the physical-mathematical and computational models of the flow in the air intake. The air flow is modeled as a mixture of perfect gases taking into account the dependence of thermodynamic properties on the temperature and pressure. The paper provides the results of comparing the calculated data obtained for flight conditions and bench tests.
One-Dimensional Model for Calculation of Flow Parameters in a Supersonic Air Intake
Russ. Aeronaut.
Russian Aeronautics ; 66 , 3 ; 528-533
2023-08-01
6 pages
Article (Journal)
Electronic Resource
English
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