Integrated inward turning inlets and nozzles for hypersonic...

Aeronautics and astronautics – Aircraft power plants

Reexamination Certificate

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Reexamination Certificate

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07866599

ABSTRACT:
A hypersonic waverider aircraft is disclosed that includes a first engine and an inlet including a throat. The inlet is configured to generate three-dimensional flow compression during hypersonic flight with a weak shock wave that begins at the leading edge surfaces of the inlet and coalesces ahead of the throat, and a weak shock wave that begins at the point of coalescence of the weak shock wave and extends to the throat. The inlet includes a v-shaped lip open to freestream airflow in one side of the inlet.

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