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一前言空对空导弹外挂飞行时的气动加热对于导弹的设计与使用是个很重要的问题。当载机飞行加速越来越高时更是如此,往往需要根据气动加热温度在设计中考虑绝热措施,或者由于导弹受热能力有限而限制载机飞行马赫数。
A Preamble Aerodynamic heating of an air-to-air missile plug-in flight is a very important issue for the design and use of missiles. This is particularly the case when the flight speed of the carrier aircraft is getting higher and higher, and it is often necessary to consider the adiabatic measures in the design according to the aerodynamic heating temperature, or to limit the Mach-number of the carrier flight due to the limited heat capacity of the missile.