Theoretical fundamentals of airframe/propulsion integration for high-speed aircraft

被引:1
|
作者
Gubanov, A. A. [1 ]
机构
[1] Cent Aerohydrodynam Inst, Zhukovskii, Moscow Region, Russia
关键词
Aircraft aerodynamics; Supersonic flight vehicles; Aerodynamic configurations; Airframe; propulsion integration; Analytical studies; CFD; Wind-tunnel tests;
D O I
10.1186/s42774-019-0013-8
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
Fundamental features of aerodynamic interference and integration of airframes and air-breathing jet engines for high-speed flight vehicles are studied within the framework of supersonic small perturbation theory. Both the influence of airframe components on air intakes performance and influence of intakes on vehicle external aerodynamics are under consideration. Analytical relations and specific examples show that significant favorable interference between airframes and air intakes can be realized by using preliminary compression of the flow in front of intakes at flight Mach numbers exceeding approximately 3.
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页数:13
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