Preliminary evaluation of the performance of a uniflow two-stroke-cycle spark-ignition engine combined with a blowdown turbine and a steady-flow turbine
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Sather, Bernard I↗
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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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Cooling of gas turbine III : analysis of rotor and blade temperature in liquid-cooled gas turbine
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Brown, W Byron↗
Cooling of gas turbine IV : calculated temperature distribution in the trailing part of a turbine blade using direct liquid cooling
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Brown, W Byron↗
Cooling of gas turbines VI : computed temperature distribution through cross section of water-cooled turbine blade
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Livingood, John N↗
Cooling of gas turbines VIII : theoretical temperature distributions through gas turbine with special blades and cooling fins on the rim
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Brown, W Byron↗
Turbine-rotor-blade Designs Based on One-dimensional-flow Theory I : Performance of Single-stage Turbine Having 40-percent Reaction
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English, Robert E↗
Vibrational Modes of Several Hollow Turbine Blades and of Solid Turbine Blade of Similar Aerodynamic Design
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Kemp, R H↗
Turbine Performance Characteristics of a Python Turbine-propeller Engine Investigated in Altitude Wind Tunnel
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Farley, John M↗
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↗
Investigation of turbines suitable for use in a turbojet engine with high compressor pressure ratio and low compressor tip-speed II : velocity-diagram study of turbine for engine operation with constant exhaust-nozzle area
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Davison, Elmer H↗
Investigation of turbines suitable for use in a turbojet engine with high compressor pressure ratio and low compressor-tip speed III : velocity-diagram study of two-stage and downstream-stator turbines for engine operation at constant rotative speed
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English, Robert E↗
Investigation of turbines suitable for use in a turbojet engine with high compressor pressure ratio and low compressor-tip speed IV : effect of increasing blade speed on velocity diagrams of turbine for engine operation at constant rotative speed
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Davison, Elmer H↗
Turbine design considerations for turbine-propeller engine operating over a range of flight conditions
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Davison, Elmer H↗
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 Evaluation of Reduced-chord Rotor Blading as Applied to J73 Two-stage Turbine IV : Over-all Performance of First-stage Turbine with Reduced-chord Rotor Blades at Inlet Conditions of 35 Inches of Mercury Absolute and 700 R
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Schum, Harold J↗
Analysis of factors affecting selection and design of air-cooled single-stage turbine for turbojet engines I : turbine performance and engine weight-flow capacity
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Rossbach, Richard J↗
Investigation of Rotating Components of Counterrotating Two-spool Engines I : Analytical Investigation of Off-design Performance of Turbine Component Designed with and Without Outer-turbine Stator
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Steward, Warner L↗
Effects of Turbine Cooling with Compressor Air Bleed on Gas-turbine Engine Performance
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Esgar, Jack B↗