An engine inlet for efficient operation at both design Mach number and off-design Mach numbers with an inlet having a caret configuration with rotatably extending effective leading edges on the inlet from a retracted position aligned with a nominal Mach number shock wave to an extended position aligned with an off-design Mach number shock wave.
SUPERSONIC CARET INLET SYSTEM LEADING EDGE SLAT FOR IMPROVED INLET PERFORMANCE AT OFF-DESIGN FLIGHT CONDITIONS
29.12.2016
Patent
Elektronische Ressource
Englisch
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