Browse TRAIL Inventories

Investigation of Slipstream Effects on a Wing-Inlet Oil-Cooler Ducting System of a Twin-Engine Airplane in the Ames 40- by 80-Foot Wind Tunnel

Experimental investigation of the effects of viscosity on the drag of bodies of revolution at a Mach number 1.5

Experimental investigation of the effects of viscosity on the drag and base pressure of bodies of revolution at a Mach number 1.5

Laminar mixing of a compressible fluid

Laminar mixing of a compressible fluid

Reduction of profile drag at supersonic velocities by the use of airfoil sections having a blunt trailing edge


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