Search U.S. government technical reports digitized or harvested by TRAIL.
Knock-Limited Blending Characteristics of Blends of Triptane and 28-R Aviation Fuel
The effects of yawing thin pointed wings at supersonic speeds
Distribution of wave drag and lift in the vicinity of wing tips at supersonic speeds
The use of perforated inlets for efficient supersonic diffusion
Theoretical Lift Distribution and Upwash Velocities for Thin Wings at Supersonic Speeds
Theoretical distribution of lift on thin wings at supersonic speeds (An extension)
Investigation of a variable Mach number supersonic tunnel with nonintersecting characteristics