A wave rider is a configuration designed such that the bow shock generated by the shape is perfectly attached along the leading edge at the design condition.
乘波体是一种由已知超声速或高超声速流场生成的气动构形,在设计点乘波体构型的整个前缘产成贴附的激波。
The attached leading-edge shock wave confines the high-pressure region to the low surface.
经过激波后的高压流动被限制在下表面,并且流场非常均匀。
This method may be used to calculate the arbitrary airfoils with sharp leading edge provided that the shock wave is attached.
在激波附体的条件下,本文的方法可用于计算大迎角尖前缘任意翼型的超音速和高超音速俯仰安定性导数。
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