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Heat-transfer Tests of a Steel Cylinder Barrel with Aluminum Fins
High-altitude Cooling III : Radiators
High-altitude cooling I : resume of the cooling problem
Investigation of Aircraft Heaters. 25 - Use of the Thermopile Radiometer
Nitrous oxide supercharging of an aircraft-engine cylinder
Cooling of a Double-row Radial Engine by Water Injection to the Individual Cylinders
An analysis of supersonic aerodynamic heating with continuous fluid injection
Structural Design for Aerodynamic Heating. Part II. Analytical Studies
Free-flight investigations of subliming ablators and transpiration cooling at hypersonic velocities
Investigation of Cooling Problems at High Chamber Pressures Final Report, 1 Jul. 1963 - 31 Mar. 1965
Investigation of Cooling Problems at High Chamber Pressures Final Report, 1 Jul. 1963 - 31 Mar. 1965
A radiation-cooled nuclear rocket nozzle for long firing durations.
A large ultrahigh-vacuum environmental chamber with liquid-helium-cooled liner.
Analytical Study of Moderator Wall Cooling of Gaseous Nuclear Rocket Engines
Beryllium Fabrication Methods Development Program - Thermal Treatment
Experimental Snow Plenum Air Cooling System for Byrd Station, Antarctica
Silent, 3.75 KW Liquid Hydrocarbon-Air Fuel Cell Powerplant. Volume II. Figures and Tables
Air Heating by a Rotating Arc with Cold Gas Flow Transverse to the Axis of the Arc
Gaseous-film cooling of a rocket motor with injection near the throat
Thermal Insulation of Small Instrumentation Probes
Evaluation of an Infrared Heating Simulation of a Mach 4.63 Flight on an X 15 Horizontal Stabilizer
The Influence of Gravity on Heat Transfer in Heat Pipes
Heatpipes and Vapor Chambers for Satellite Thermal Balance
Investigation of External Refrigeration Systems for Long Term Cryogenic Storage
Inflatable, Transpiration Cooled Nozzle Patent Application
Study of Transformations in T-A6V Titanium Alloy under Continuous Cooling
Airflow Rate Requirements in Passenger Aircraft
A Laboratory Comparison of Three Methods of Personal Conditioning
A Laboratory Comparison of Three Methods of Personal Conditioning
Design of a Convective Cooling System for a Mach 6 Hypersonic Transport Airframe
Aerocooling of a 12-Inch Diameter Missile During Air Carry
OSS-1: A Pathfinder Mission for Space Science on Shuttle
Propulsion Apparatus and Method Using Boil-off Gas from a Cryogenic Liquid
Three-dimensional thermal modeling of electric vehicle batteries