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.
Hypersonic waverider stream surface actuation for variable design point operation
2022-05-10
Patent
Electronic Resource
English
Hypersonic Waverider Stream Surface Actuation for Variable Design Point Operation
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