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
23.01.2018
Patent
Elektronische Ressource
Englisch
Europäisches Patentamt | 2022
Europäisches Patentamt | 2017
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