SNAP-8 Development Status von Slone, Henry O

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Analysis of coolant flow and pressure requirements for a return-flow turbine rotor blade design using hydrogen, helium, or air as coolant von Slone, Henry O, Donoughe, Patrick L

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Gas-turbine-engine performance when heat from liquid-cooled turbines is rejected ahead of, within, or behind main compressor von Esgar, Jack B, Slone, Henry O

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GAS-TO-BLADE HEAT-TRANSFER COEFFICIENTS AND TURBINE HEAT-REJECTION RATES FOR A RANGE OF ONE-SPOOL COOLED-TURBINE ENGINE DESIGNS von SLONE, HENRY O, ESGAR, JACK B

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Gas-to-blade heat-transfer coefficients and turbine heat-rejection rates for a range of one-spool cooled-turbine engine designs von Slone, Henry O, Esgar, Jack B

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Analysis of Cooling-air Requirements of Corrugated-insert-type Turbine Blades Suitable for a Supersonic Turbojet Engine von Ziemer, Robert R, Slone, Henry O

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Analytical comparison of convection-cooled turbine blade cooling-air requirements for several radial gas-temperature profiles von Hubbartt, James E, Slone, Henry O

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Analysis of Factors Affecting Selection and Design of Air-cooled Single-stage Turbines for Turbojet Engines IV : Coolant-flow Requirements and Performance of Engines Using Air-cool... von Slone, Henry O, Hubbartt, James E

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Analytical Procedures for Rapid Selection of Coolant Passage Configurations for Air-cooled Turbine Rotor Blades and for Evaluation of Heat-transfer, Strength, and Pressure-loss Cha... von Ziemer, Robert R, Slone, Henry O

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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... von Slone, Henry O, Cochran, Reeves P, Dengler, Robert P

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Method of Designing Corrugated Surfaces Having Maximum Cooling Effectiveness Within Pressure-drop Limitations for Application to Cooled Turbine Blades von Slone, Henry O, Hubbartt, James E, Arne, Vernon L

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Method for Rapid Determination of Pressure Change for One-Dimensional Flow with Heat Transfer, Friction, Rotation, and Area Change von Hubbartt, James E, Slone, Henry O, Arne, Vernon L

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Procedure for calculating turbine blade temperatures and comparison of calculated with observed values for two stationary air-cooled blades von Richards, Hadley T, Slone, Henry O, Brown, W Byron

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A 20,000-Kilowatt Nuclear Turboelectric Power Supply for Manned Space Vehicles von English, Robert E., Slone, Henry O., Bernatowicz, Daniel T., Davison, Elmer H., Lieblein, Seymour

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