One-Dimensional Model for Calculation of Flow Parameters in a Supersonic Air Intake

被引:0
|
作者
Gidaspov V.Y. [1 ]
Moseev D.S. [1 ]
Severina N.S. [1 ]
机构
[1] Moscow Aviation Institute (National Research University), Volokolamskoe sh. 4, Moscow
来源
Russian Aeronautics | 2023年 / 66卷 / 3期
关键词
air intake; high-velocity flow; multicomponent gas; propulsion system; total pressure coefficient;
D O I
10.3103/S1068799823030145
中图分类号
学科分类号
摘要
Abstract: 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. © 2023, Allerton Press, Inc.
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页码:528 / 533
页数:5
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