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.

中文翻译：

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高速飞机机身/推进系统集成的理论基础

在超音速小扰动理论的框架内研究了空气动力干扰的基本特征以及高速飞行器的机身与空气呼吸喷气发动机的集成。机身部件对进气性能的影响以及进气对车辆外部空气动力学的影响都在考虑之中。解析关系和具体示例表明，在飞行马赫数超过约3时，通过对进气口前面的流进行预压缩，可以实现机身和进气口之间的显着有利干扰。