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Abkühlen
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Advanced and Additive Manufacturing Technologies for Liquid Rocket Engine Components
Altitude Performance Characteristics of Tail-pipe Burner with Variable-area Exhaust Nozzle
A Method for the Design of Cooling Systems for Aircraft Power-plant Installations
A Method for Welding Sheet Aluminum to SAE 4140 Steel
Analytical solution of the ''known-heat-load'' space radiator problem.
An analysis of supersonic aerodynamic heating with continuous fluid injection
AN EXPERIMENTAL INVESTIGATION OF GASEOUS-FILM COOLING OF A ROCKET MOTOR
An experimental investigation of rectangular exhaust-gas ejectors applicable for engine cooling
A Preliminary Investigation of Exhaust-gas Ejectors for Ground Cooling
A radiation-cooled nuclear rocket nozzle for long firing durations.
A Summary of Drag Results from Recent Langley Full Scale Tunnel Tests of Army and Navy Airplanes
Construction of Finned Aluminum Muffs for Aircraft Engine Cylinder Barrels
Continuous use of internal cooling to suppress knock in aircraft engines cruising at high power