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Results for “TURBINE”

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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At least 145 records · Page 8

All sources NASA NTRS DOE OSTI

NASA NTRS1952

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↗

NASA NTRS1952

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↗

NASA NTRS1953

Turbine design considerations for turbine-propeller engine operating over a range of flight conditions

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Davison, Elmer H↗

NASA NTRS1953

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↗

NASA NTRS1957

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↗

NASA NTRS1954

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↗

NASA NTRS1955

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↗

NASA NTRS1955

Effects of Turbine Cooling with Compressor Air Bleed on Gas-turbine Engine Performance

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Esgar, Jack B↗

NASA NTRS1956

Component performance investigation of J71 experimental turbine V : effect of third stage shrouding on internal-flow conditions of J71-97 turbine

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Petrash, Donald A↗

NASA NTRS1956

Experimental Investigation of Air-cooled Turbine Rotor Blade Temperatures in a Turbojet Engine Operating at Turbine-inlet Temperatures up to 2580 Degrees R and Altitudes of 50,000 and 60,000 Feet

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Slone, Henry O↗

NASA NTRS1956

Temperature-control study of turbine region of turbojet engine, including turbine-blade time constants and starting characteristics

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Phillips, W E , Jr↗

NASA NTRS1956

Component Performance Investigation of J71 Experimental Turbine VI : Effect of First-stator Adjustment; Over-all Performance of J71-97 Turbine with 70-percent-design Stator Area

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Schum, Harold J↗

NASA NTRS1957

Investigation of a 0.6 hub-tip radius-ratio transonic turbine designed for secondary-flow study I : design and experimental performance of standard turbine

Detailed design information including overall performance parameters, velocity diagrams, and blade surface velocities is presented. Experimental performance includes maps based on rating as well as total-pressure ratios showing the effect of exit whirl. Also included are results of surveys at the stator exit and downstream of the rotor at design speed and specific work. This information will be used as a standard for comparison with subsequent secondary-flow work.

Rohlik, Harold E↗

NASA NTRS1957

Component Performance Investigation of J71 Experimental Turbine IX : Effect of First-stator Adjustment;internal Flow Conditions of J71-97 Turbine with 87-percent-design Stator Area

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Schum, Harold J↗

NASA NTRS1957

Investigation of a 0.6 Hub-tip Radius-ratio Transonic Turbine Designed for Secondary-flow Study II : Design and Experimental Performance of Turbine with Low-velocity-turning Stator and Standard Rotor

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Rohlik, Harold E↗

NASA NTRS1958

Component Performance Investigation of J71 Experimental Turbine X : Effect of First-stator Adjustment; Internal Flow Conditions of J71-97 Turbine with 132-percent-design Stator Area

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Petrash, Donald A↗

NASA NTRS1956

Gas-turbine-engine performance when heat from liquid-cooled turbines is rejected ahead of, within, or behind main compressor

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Esgar, Jack B↗

NASA NTRS1957

Investigation of turbines suitable for use in a turbojet engine with high compressor pressure ratio and low compressor-tip speed VIII : internal flow conditions of a two-stage turbine with a downstream stator

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Petrash, Donald A↗