COMPLIANT INTERMEDIATE COMPONENT OF A GAS TURBINE ENGINE
Stress mitigation feature for composite airfoil leading edge
Turbine engine assembly and method of manufacturing thereof
TURBINE ENGINE ASSEMBLY AND METHOD OF MANUFACTURING THEREOF
TURBINE ENGINE ASSEMBLY AND METHOD OF MANUFACTURING THEREOF
Turbine engine assembly and method of manufacturing thereof
Turbomachine casing comprising a cavity-free shroud and yokes reinforced by stiffeners