Analysis of coolant flow and pressure requirements for a return-flow turbine rotor blade design using hydrogen, helium, or air as coolant
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Slone, Henry O↗
Engineering topics
Slone, Henry O
Publications and source records attributed to Slone, Henry O.
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↗
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↗
Gas-to-blade heat-transfer coefficients and turbine heat-rejection rates for a range of one-spool cooled-turbine engine designs
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Slone, Henry O↗
Analysis of Cooling-air Requirements of Corrugated-insert-type Turbine Blades Suitable for a Supersonic Turbojet Engine
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Ziemer, Robert R↗
Analytical comparison of convection-cooled turbine blade cooling-air requirements for several radial gas-temperature profiles
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Hubbartt, James E↗
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-cooled Corrugated-insert Blades
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Slone, Henry O↗
Method of Designing Corrugated Surfaces Having Maximum Cooling Effectiveness Within Pressure-drop Limitations for Application to Cooled Turbine Blades
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Slone, Henry O↗
Method for Rapid Determination of Pressure Change for One-Dimensional Flow with Heat Transfer, Friction, Rotation, and Area Change
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Hubbartt, James E↗
Procedure for calculating turbine blade temperatures and comparison of calculated with observed values for two stationary air-cooled blades
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Richards, Hadley T↗
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 Characteristics
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Ziemer, Robert R↗