Browse TRAIL Inventories

Aerodynamic characteristics at subcritical and supercritical Mach numbers of two airfoil sections having sharp leading edges and extreme rearward positions of maximum thickness

One-Dimensional Flows of an Imperfect Diatomic Gas

Approximate methods for calculating the flow about nonlifting bodies of revolution at high supersonic airspeeds

A unified two-dimensional approach to the calculation of three-dimensional hypersonic flows, with application to bodies of revolution

On the calculation of flow about objects traveling at high supersonic speeds

Bodies of Revolution for Minimum Drag at High Supersonic Airspeeds

Inviscid Flow About Airfoils at High Supersonic Speeds

A Study of Inviscid Flow About Airfoils at High Supersonic Speeds

The Ames 10- by 14-Inch Supersonic Wind Tunnel

A method for simulating the atmospheric entry of long-range ballistic missiles

A method for simulating the atmospheric entry of long-range ballistic missiles

Bodies of revolution having minimum drag at high supersonic airspeeds

Experimental Investigation of a Body Flare for Obtaining Pitch Stability and a Body Flap for Obtaining Pitch Control in Hypersonic Flight

Initial Experiments on the Aerodynamic Cooling Associated With Large-Scale Vortical Motions in Supersonic Flow

Experimental investigation of a body flare for obtaining pitch stability and a body flap for obtaining pitch control in hypersonic flight

Theoretical and Experimental Investigation of the Effect of Yaw on Heat Transfer to Circular Cylinders in Hypersonic Flow

Bodies of revolution having minimum drag at high supersonic airspeeds

Aircraft configurations developing high lift-drag ratios at high supersonic speeds

Stagnation-point heat transfer to blunt shapes in hypersonic flight, including effects of yaw


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