Browse TRAIL Inventories

An Estimation of the Internal-Cooling Requirements of an Aircraft-Engine Cylinder When Using Oxygen Boost

Knock-Limited Blending Characteristics of Blends of Triptane and 28-R Aviation Fuel

A correlation of the effects of compression ratio and inlet-air temperature on the knock limits of aviation fuels in a CFR engine 1

A relation between knock-limited or preignition-limited air-fuel ratio at lean mixtures and fuel-air ratio at rich mixtures

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

A linearized solution for time-dependent velocity potentials near three-dimensional 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

Use of source distributions for evaluating theoretical aerodynamics of thin finite wings at supersonic speeds

Three-dimensional supersonic nozzles and inlets of arbitrary exit cross section

The use of perforated inlets for efficient supersonic diffusion


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