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Journal Articles

Highlights of Roy Smith’s Career at General Electric

C. C. Koch
Journal: Journal of Turbomachinery
Publisher: ASME
Article Type: Special Section: Honoring Dr. Leroy H. Smith
J. Turbomach. November 2012, 134(6): 060901.
https://doi.org/10.1115/1.4007209
Published Online: September 19, 2012
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Topics: Compressors, Design, Engines
Proceedings Papers

Highlights of Roy Smith’s Career at GE

C. C. Koch
Proc. ASME. GT2009, Volume 7: Turbomachinery, Parts A and B, 795-800, June 8–12, 2009
Publisher: American Society of Mechanical Engineers
Paper No: GT2009-60369
https://doi.org/10.1115/GT2009-60369
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Topics: Compressors, Design theory, Engines, Gas turbines, International Gas Turbine Institute, Jet engines, Turbochargers
Journal Articles

Stalling Pressure Rise Capability of Axial Flow Compressor Stages

C. C. Koch
Journal: Journal of Engineering for Gas Turbines and Power
Publisher: ASME
Article Type: Research Papers
J. Eng. Gas Turbines Power. October 1981, 103(4): 645–656.
https://doi.org/10.1115/1.3230787
Published Online: October 1, 1981
View Article titled, Stalling Pressure Rise Capability of Axial Flow Compressor Stages
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Topics: Axial flow, Pressure, Compressors, Fluids, Geometry, Reynolds number, Airfoils, Boundary layers, Cascades (Fluid dynamics), Clearances (Engineering)
Journal Articles

Discussion: “Experimental and Analytical Investigation of the Effects of Reynolds Number and Blade Surface Roughness on Multistage Axial Flow Compressors” (Scha¨ffler, A., 1980, ASME J. Eng. Power, 102, pp. 5–12)

C. C. Koch, L. H. Smith, Jr.
Journal: Journal of Engineering for Gas Turbines and Power
Publisher: ASME
Article Type: Discussions
J. Eng. Gas Turbines Power. January 1980, 102(1): 12.
https://doi.org/10.1115/1.3230208
Published Online: January 1, 1980
View Article titled, Discussion: “Experimental and Analytical Investigation of the Effects of Reynolds Number and Blade Surface Roughness on Multistage Axial Flow Compressors” (Scha¨ffler, A., 1980, ASME J. Eng. Power, 102, pp. 5–12)
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Topics: Axial flow, Blades, Compressors, Reynolds number, Surface roughness
Journal Articles

Closure to “Discussion of ‘Loss Sources and Magnitudes in Axial-Flow Compressors’” (1977, ASME J. Eng. Power, 99, p. 297)

C. C. Koch, L. H. Smith, Jr.
Journal: Journal of Engineering for Gas Turbines and Power
Publisher: ASME
Article Type: Discussions
J. Eng. Gas Turbines Power. April 1977, 99(2): 297.
https://doi.org/10.1115/1.3446290
Published Online: April 1, 1977
View Article titled, Closure to “Discussion of ‘Loss Sources and Magnitudes in Axial-Flow Compressors’” (1977, ASME J. Eng. Power, 99, p. 297)
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Topics: Axial flow
Journal Articles

Loss Sources and Magnitudes in Axial-Flow Compressors

C. C. Koch, L. H. Smith, Jr.
Journal: Journal of Engineering for Gas Turbines and Power
Publisher: ASME
Article Type: Research Papers
J. Eng. Gas Turbines Power. July 1976, 98(3): 411–424.
https://doi.org/10.1115/1.3446202
Published Online: July 1, 1976
View Article titled, Loss Sources and Magnitudes in Axial-Flow Compressors
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Topics: Axial flow, Compressors, Design, Airfoils, Annulus, Boundary layers, Finishes, Fluids, Hardware, Mach number