An aircraft includes an airframe, an engine mounted to the airframe, and an engine inlet for receiving an ambient airflow and providing the ambient airflow to the engine. An amount of airflow provided to the engine inlet is controllable.
VARIABLE GEOMETRY ENGINE INLET FOR HIGH SPEED AIRCRAFT
EINLASS MIT VARIABLER GEOMETRIE FÜR HOCHGESCHWINDIGKEITSFLUGZEUGE
ENTRÉE DE MOTEUR À GÉOMÉTRIE VARIABLE POUR AVION À GRANDE VITESSE
2021-03-17
Patent
Elektronische Ressource
Englisch
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