AIRCRAFT HYBRID MOTIVE POWER SOURCE SYSTEM AND METHOD FOR CONTROLLING SAME
COMPOUND TYPE VESSEL HYBRID POWER SYSTEM BASED ON AMMONIA-HYDROGEN DRIVE
DETECTABLE DATUM MARKERS FOR GAS TURBINE ENGINE COMPONENTS FOR MEASURING DISTORTION
LIQUID-IMPREGNATED SURFACES, METHODS OF MAKING, AND DEVICES INCORPORATING THE SAME
METHODS AND APPARATUS FOR FORMING APERTURE IN COMPOSITE COMPONENT
METHODS AND APPARATUS TO MODEL THERMAL MIXING FOR PREDICTION OF MULTI-STREAM FLOWS