Aspects of the disclosure are directed to a system of an aircraft, comprising: at least one fairing, a liner, and an actuator configured to cause the at least one fairing to be translated relative to the liner in order to obtain a modulation of a metering area between the liner and the at least one fairing,
STEPPED FAIRING MODULATED EXHAUST COOLING
16.06.2016
Patent
Elektronische Ressource
Englisch