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J. L. Allen
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Journal Articles

Discussion: “Avon No. 8—A Supercritical-Pressure Plant” (Dauber, C. A., 1957, Trans. ASME, 79, pp. 927–936)

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J. L. Allen
Journal: Journal of Fluids Engineering
Publisher: ASME
Article Type: Discussions
J. Fluids Eng. May 1957, 79(4): 936.
https://doi.org/10.1115/1.4013195
Published Online: February 14, 2022
View Articletitled, Discussion: “Avon No. 8—A Supercritical-Pressure Plant” (Dauber, C. A., 1957, Trans. ASME, 79, pp. 927–936)
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Topics: Pressure
Journal Articles

The Development of Fast Response Aerodynamic Probes for Flow Measurements in Turbomachinery

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R. W. Ainsworth, J. L. Allen, J. J. M. Batt
Journal: Journal of Turbomachinery
Publisher: ASME
Article Type: Research Papers
J. Turbomach. October 1995, 117(4): 625–634.
https://doi.org/10.1115/1.2836581
Published Online: October 1, 1995
View Articletitled, The Development of Fast Response Aerodynamic Probes for Flow Measurements in Turbomachinery
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Topics: Flow measurement, Probes, Turbomachinery, Semiconductors (Materials), Design, Flow (Dynamics), Transients (Dynamics), Turbines, Lasers, Mach number
Journal Articles

Developments in Instrumentation and Processing for Transient Heat Transfer Measurement in a Full-Stage Model Turbine

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R. W. Ainsworth, J. L. Allen, M. R. D. Davies, J. E. Doorly, C. J. P. Forth, M. A. Hilditch, M. L. G. Oldfield, A. G. Sheard
Journal: Journal of Turbomachinery
Publisher: ASME
Article Type: Research Papers
J. Turbomach. January 1989, 111(1): 20–27.
https://doi.org/10.1115/1.3262232
Published Online: January 1, 1989
View Articletitled, Developments in Instrumentation and Processing for Transient Heat Transfer Measurement in a Full-Stage Model Turbine
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Topics: Instrumentation, Transient heat transfer, Turbines, Cascades (Fluid dynamics), Generators, Pistons, Rotors, Tunnels, Wakes
Journal Articles

A Study of the Effects of Thermal Barrier Coating Surface Roughness on the Boundary Layer Characteristics of Gas Turbine Aerofoils

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R. M. Watt, J. L. Allen, N. C. Baines, J. P. Simons, M. George
Journal: Journal of Turbomachinery
Publisher: ASME
Article Type: Research Papers
J. Turbomach. January 1988, 110(1): 88–93.
https://doi.org/10.1115/1.3262172
Published Online: January 1, 1988
View Articletitled, A Study of the Effects of Thermal Barrier Coating Surface Roughness on the Boundary Layer Characteristics of Gas Turbine Aerofoils
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Topics: Airfoils, Boundary layers, Gas turbines, Surface roughness, Thermal barrier coatings, Cascades (Fluid dynamics), Reynolds number, Design, Nozzle guide vanes, Polishing