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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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At least 289 records · Page 16

All sources NASA NTRS DOE OSTI

NASA NTRS1952

Preliminary air-flow and thrust calibrations of several conical Cooling-air ejectors with a primary to secondary temperature ratio of 1.0 I : diameter ratios of 1.21 and 1.10

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Greathouse, W K↗

NASA NTRS1953

Performance of double-shroud ejector configuration with primary pressure ratios from 1.0 to 10

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Hollister, Donald P↗

NASA NTRS1953

Air-flow and thrust characteristics of several cylindrical cooling-air ejectors with a primary to secondary temperature ratio of 1.0

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Greathouse, W K↗

NASA NTRS1954

Effects of Auxiliary and Ejector Pumping on the Mach Number Attainable in a 4 1/2- by 4 1/2- Inch Slotted Tunnel at Low Pressure Ratios

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Dennard, John S↗

NASA NTRS1954

Effect of properties of primary fluid on performance of cylindrical shroud ejectors

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Kochendorfer, Fred D↗

NASA NTRS1953

Performance characteristics of a double-cylindrical-shroud ejector nozzle

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Reshotko, Eli↗

NASA NTRS1954

Preliminary Investigation of Pumping and Thrust Characteristics of Full-size Cooling-air Ejectors at Several Exhaust-gas Temperatures

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Greathouse, W K↗

NASA NTRS1954

Experimental Data for Four Full-scale Conical Cooling-air Ejectors

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Ciepluch, C C↗

NASA NTRS1954

Note on performance of aircraft ejector nozzles at high secondary flows

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Kochendorfer, Fred D↗

NASA NTRS1954

Thrust and Pumping Characteristics of a Series of Ejector-type Exhaust Nozzles at Subsonic and Supersonic Flight Speeds

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Hearth, Donald P↗

NASA NTRS1954

Pumping characteristics for several simulated variable-geometry ejectors with hot and cold primary flow

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Allen, John L↗

NASA NTRS1955

Effect of free-stream Mach number on gross-force and pumping characteristics of several ejectors

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Stitt, Leonard E↗

NASA NTRS1955

Effect on Ejector Performance of Varying Diameter Ratio by Simulated Iris Flaps

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Valerino, Alfred S↗

NASA NTRS1955

Matching of Auxiliary Inlets to Secondary-air Requirements of Aircraft Ejector Exhaust Nozzles

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Hearth, Donald P↗

NASA NTRS1955

Investigation at Supersonic Speeds of External-drag Effects and Pumping Characteristics of a Short Ejector

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Love, Eugene S↗

NASA NTRS1955

Effects of combining auxiliary bleed with ejector pumping on the power requirements and test-section flow of an 8-inch by 8-inch slotted tunnel

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Little, B H , Jr↗

NASA NTRS1955

Performance characteristics of several divergent-shroud aircraft ejectors

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Greathouse, William K↗

NASA NTRS1956

External-stream effects on gross thrust and pumping characteristics of ejectors operating at off-design Mach numbers

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Valerino, Alfred S↗