A systematic investigation of pressure distributions at high speeds over five representative NACA low-drag and conventional airfoil sections
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Graham, Donald J↗
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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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Effects of Compressibility on the Characteristics of Five Airfoils
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Daley, Bernard N↗
Combustion-efficiency and altitude-limit investigations of five fuels in an annular turbojet combustor
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Wear, Jerrold D↗
Sound measurements for five shrouded propellers at static conditions
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Hubbard, Harvey H↗
Flight Determined Buffet Boundaries of Ten Airplanes and Comparisons with Five Buffeting Criteria
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Gadeberg, Burnett L↗
Aerodynamics of Slender Bodies at Mach Number of 3.12 and Reynolds Numbers from 2 x 10(exp 6) to 15 x 10(exp 6) II : Aerodynamic Load Distributions of Series of Five Bodies Having Conical Noses and Cylindrical Afterbodies
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Jack, John R↗
Performance of pure fuels in a single J33 combustor I : five liquid hydrocarbon fuels
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Wear, Jerrold D↗
An Analysis of Pressure Studies and Experimental and Theoretical Downwash and Sidewash Behind Five Pointed-tip Wings at Supersonic Speeds
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Boatright, William B↗
Experimental Investigation of a Five-stage Axial-flow Research Compressor with Transonic Rotors in All Stages II : Compressor Over-all Performance
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Kovach, Karl↗
Effect of Fuel Additives on Carbon Deposition in a J33 Single Combustor III : Five Organo-metallic Additives
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Jonash, Edmund R↗
Static lateral-directional stability characteristics of five contemporary airplane models from wind-tunnel tests at high subsonic and supersonic speeds
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Smith, Willard G↗
Performance of pure fuels in a single J33 combustor III : five hydrocarbon gaseous fuels and one oxygenated hydrocarbon gaseous fuel
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Smith, Arthur L↗
Turbojet Engine Investigation of Effect of Thermal Shock Induced by External Water-spray Cooling on Turbine Blades of Five High-temperature Alloys
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Freche, John C↗
An experimental study of five annular air inlet configurations at subsonic and transonic speeds
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Pendley, Robert E↗
Performance of Five Low-temperature-ratio Ram-jet Combustors over Range of Simulated Altitudes
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Wentworth, Carl B↗
Statistical measurements of landing contact conditions of five military airplanes during routine daytime operations
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Silsby, Norman S↗
Experimental investigation of a five-stage axial-flow research compressor with transonic rotors in all stages IV : blade-element performance
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Sandercock, Donald M↗
Experimental Investigation of a Five-stage Axial-flow Research Compressor with Transonic Rotors in All Stages III : Interstage Data and Individual Stage Performance Characteristics
For use in computing the detailed performance parameters of individual blade rows of a multistage compressor, radial distributions of total pressure, total temperature, static pressure and air-flow angle are tabulated. The data cover a range of air flow from choke to the approximate surge limit for equivalent rotor speeds from 70 to 100 percent of design. Equivalent stage performance curves determined from the radial survey measurements indicate both the individual performance and the matching of the stages at the speeds investigated.
Sandercock, Donald M↗