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Kühlsystem
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Advanced and Additive Manufacturing Technologies for Liquid Rocket Engine Components
A large ultrahigh-vacuum environmental chamber with liquid-helium-cooled liner.
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 probe for total-enthalpy measurements in arcjet exhausts.
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
Clock Technology Development for the Laser Cooling and Atomic Physics (LCAP) Program
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
Cooling of a Double-row Radial Engine by Water Injection to the Individual Cylinders
Cowling and Cooling Tests of a Fleetwings Model 33 Airplane in Flight
Cyrogenic Life Support Technology Development Project
Design, Selection, and Installation of Aircraft Heat Exchangers
Devices for controlling thermal gradients in spacecraft structures
Drag Analysis of Single-Engine Military Airplanes Tested in the NACA Full-Scale Wind Tunnel
Economy of internally cooling only the overheated cylinders of aircraft engines
Effect of Exhaust Pressure on the Cooling Characteristics of an Air-cooled Engine
Effect of Oil Flow to Piston on Piston-ring Sticking and Oil Consumption in a Single-cylinder Engine
Engine Tests of Pressurized Shunt-type Cooling Systems for a Liquid-cooled Engine
Experimental investigation of a lightweight rocket chamber
Free-flight investigations of subliming ablators and transpiration cooling at hypersonic velocities
Full-Scale Wind-Tunnel Investigation of Forward Underslung Cooling-Air Ducts