Cooling of ram jets and tail-pipe burners : analytical method for determining temperatures of combustion chamber having annular cooling passage
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Koffel, William K↗
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Results for “cooling”
Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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Experimental investigation of air-cooled turbine blades in turbojet engine III : rotor blades with 34 steel tubes in cooling-air passages
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Hickel, Robert O↗
Experimental investigation of air-cooled turbine blades in turbojet engine II : rotor blades with 15 fins in cooling-air passages
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Hickel, Robert O↗
Survey of advantages and problems associated with transpiration cooling and film cooling of gas-turbine blades
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Eckert, E R G↗
Experimental investigation of air-cooled turbine blades in turbojet engine VI : conduction and film cooling of leading and trailing edges of rotor blades
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Arne, Vernon L↗
Investigation of air-cooled turbine rotors for turbojet engines II : experimental cooling-air impeller performance and turbine rotor temperatures in modified J33 split-disk rotor up to speeds of 10,000 rpm
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Nachtigall, Alfred J↗
Empirical cooling correlation for an experimental afterburner with an annular cooling passage
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Koffel, William K↗
Experimental Investigation of Air-cooled Turbine Blades in Turbojet Engine XII : Cooling Effectiveness of a Blade with an Insert and with Fins Made of a Continuous Corrugated Sheet
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Bartoo, Edward R↗
Analytical comparison of turbine-blade cooling systems designed for a turbojet engine operating at supersonic speed and high altitude I : liquid-cooling systems
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Schramm, Wilson B↗
Analytical comparison of turbine-blade cooling systems designed for a turbojet engine operating at supersonic speed and high altitude II : air-cooling systems
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Schramm, Wilson B↗
Mechanical Design Analysis of Several Noncritical Air-cooled Turbine Disks and a Corrugated-insert Air-cooled Turbine Rotor Blade
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Moseson, Merland L↗
Performance of Two Air-cooled Turbojet Engines Determined Analytically from Engine Component Performance for a Range of Cooling-air Weight Flows
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Ziemer, Robert R↗
Analysis of Factors Affecting Selection and Design of Air-cooled Single-stage Turbines for Turbojet Engines IV : Coolant-flow Requirements and Performance of Engines Using Air-cooled Corrugated-insert Blades
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Slone, Henry O↗
Analytical comparison of convection-cooled turbine blade cooling-air requirements for several radial gas-temperature profiles
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Hubbartt, James E↗
Experimental Investigation of Effect of Cooling Air on Turbine Performance of Two Turbojet Engines Modified for Air-cooling
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Smith, Gordon T↗
Temperature drops through liquid-cooled turbine blades with various cooling-passage geometries
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Bartoo, Edward R↗
Cooling Characteristics of a Transpiration-cooled Afterburner with a Porous Wall of Brazed and Rolled Wire Cloth
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Koffel, William K↗
Method of Designing Corrugated Surfaces Having Maximum Cooling Effectiveness Within Pressure-drop Limitations for Application to Cooled Turbine Blades
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Slone, Henry O↗