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Hypersonic waverider stream surface actuation for variable design point operation
Hypersonic waverider stream surface actuation for variable design point operation
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机译:用于可变设计点操作的高超声速乘波器流表面驱动
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摘要
A method of designing a hypersonic vehicle includes selecting a shock shape; tracing a leading edge along the shock shape; selecting a base plane defining endpoints of the leading edge and rearwardly displaced from a front of the leading edge; and tracing stream surfaces back from the leading edge along the shock to the base plane in order to define an upper surface and a lower surface, wherein the upper and lower surfaces and base plane enclose a volume representing internal volume of the hypersonic vehicle. The lower stream surface is controllably morphable.
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