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
2018-05-08
Patent
Electronic Resource
English
European Patent Office | 2022
European Patent Office | 2017
|European Patent Office | 2020
|European Patent Office | 2018
|European Patent Office | 2016
|