Analytical comparison of convection-cooled turbine blade cooling-air requirements for several radial gas-temperature profiles
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Hubbartt, James E↗
Engineering topics
Hubbartt, James E
Publications and source records attributed to 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↗
Analysis of factors affecting selection and design of air-cooled single-stage turbines for turbojet engines III : engine design-point performance
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Rossbach, Richard J↗
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↗
Average outside surface heat-transfer coefficients and velocity distributions for heated and cooled impulse turbine blades in static cascades
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Hubbartt, James E↗
Comparison of outside-surface heat-transfer coefficients for cascades of turbine blades
A comparison of available results from heat-transfer investigations on cascades of turbine blades is presented using the Nusselt equation. The conventional correlation procedure is modified by defining the Reynolds number by the average of the velocities and the pressures around the blades. The correlation of the results from impulse blades was improved by using the Reynolds number defined by the average velocity and pressure. The final comparison indicated that several variables, which possibly influence heat transfer, should be investigated.
HEAT TRANSFER, CASCADES↗