An engine inlet 10 for efficient operation at both design Mach number and off-design Mach numbers has a fixed compression surface 16 and a leading edge 24 that is variably extendible over the fixed compression surface to simultaneously vary capture area, compression and shock wave position.
VARIABLE-CAPTURE SUPERSONIC INLET
ÜBERSCHALLEINLASS MIT VARIABLER ABSAUGUNG
ENTRÉE SUPERSONIQUE À CAPTURE VARIABLE
2021-03-10
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
Study of Supersonic Cavity Flow in Advanced Variable Geometry Inlet
Online Contents | 2005
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