Experimental Investigation of an Impulse-type Supersonic Compressor Rotor Having a Turning of 73 Degrees at the Mean Radius
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Sterrett, James R↗
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Results for “compressors”
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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Design and tests of a six-stage axial-flow compressor having a tip speed of 550 feet per second and a flat operating characteristic at constant speed
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Westphal, Willard R↗
Performance at low speeds of compressor rotors having low-cambered NACA 65-series blades with high inlet angles and low solities
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Emery, James C↗
Performance of J33 turbojet engine with shaft power extraction II : compressor
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Ross, Albert O↗
Analytical and Experimental Investigation of Thrust Augmentation of Axial- and Centrifugal-compressor Turbojet Engines by Injection of Water and Alcohol in Combustion Chambers
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Gabriel, David S↗
Investigation of the I-40 Jet-propulsion Engine in the Cleveland Altitude Wind Tunnel II : Analysis of Compressor Performance Characteristics
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Dietz, Robert O↗
Design and performance of experimental axial-discharge mixed-flow compressor I : impeller design theory
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Goldstein, Arthur W↗
Vibration Survey of NACA 24-inch Supersonic Axial-flow Compressor
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Meyer, Andre J , Jr↗
Design and Performance of Experimental Axial-discharge Mixed-flow Compressor II : Performance of Impeller
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Wilcox, Ward W↗
Investigation of performance of single-stage axial-flow compressor using NACA 5509-34 blade section
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Guentert, Donald C↗
Vibration Survey of Blades in 10-stage Axial-flow Compressor I : Static Investigation
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Meyer, Andre J , Jr↗
Vibration Survey of Blades in 10-stage Axial-flow Compressor II : Dynamic Investigation
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Meyer, Andre J , Jr↗
Vibration survey of blades in 10-stage axial-flow compressor III : preliminary engine investigation
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Meyer, Andre J , Jr↗
Calculations of the performance of a compression-ignition engine-compressor turbine combination II : performance of complete combination
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Mendelson, Alexander↗
Some methods of analyzing the effect of basic design variables on axial-flow-compressor performance
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Sinnette, John T , Jr↗
Increase in Stable-air-flow Operating Range of a Mixed-flow Compressor by Means of a Surge Inhibitor
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Laskin, Eugene B↗
Experimental investigation of thrust augmentation of 4000-pound-thrust centrifugal-flow-type turbojet engine by injection of water and alcohol at compressor inlets
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Jones, William L↗
Experimental Investigation of Thrust Augmentation of Axial-flow-type 4000-pound-thrust Turbojet Engine by Water and Alcohol Injection at Compressor Inlet
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Baron, Burnett↗