SYSTEM AND METHOD FOR CONTROLLING AN AUXILIARY POWER UNIT INLET DOOR
Stress mitigation feature for composite airfoil leading edge
AIRCRAFT PROPULSION ASSEMBLY COMPRISING AN AIR FLOW VALVE WITH A VARIABLE FLOW RATE
Aircraft propulsion assembly comprising an air flow valve with a variable flow rate
Endwall component for a turbine stage of a gas turbine engine
Endwall component for a turbine stage of a gas turbine engine
Gas turbine diffuser strut including a trailing edge flap and methods of assembling the same