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Sixty Foot Diameter Dgb Parachute Planetary Entry Parachute Program Design Report
Rotor Wake Effects on Hub/Pylon Flow. Volume I. Theoretical Formulation
Full-Scale Wind-Tunnel Study of the Effect of Nacelle Shape on Cooling Drag
Cooling Air Inlet and Exit Geometries on Aircraft Engine Installations
System Description Document for the Anthrobot-2: A Dexterous Robot Hand
Review of Ice Accretion Data from a Model Rotor Icing Test and Comparison with Theory