An engine inlet for efficient operation in both subsonic and supersonic flight wherein the inlet has a caret configuration is rotatable about an off-body axis for compression ramp angle and capture area variation and a diffuser is engaged to the inlet in a scrubbing relationship to maintain a seal upon rotation of the inlet.
SUPERSONIC CARET INLET SYSTEM
2016-09-22
Patent
Electronic Resource
English
European Patent Office | 2022
European Patent Office | 2017
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