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Some Experiences in the Scaling of the NASA 8-Stage Transonic Axial Flow Compressor Caterpillar Tractor Company

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Wiggins, J. O., author.
Conference Name:
National Farm, Construction, Industrial Machinery, Powerplant Meeting (1972-09-11 : Milwaukee, Wisconsin, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1972
Summary:
An eight-stage transonic axial flow compressor was scaled to three-tenths its original size. The scaled compressor was built and tested as a separate component, and as a component of a gas turbine engine. This paper summarizes the work done on this compressor, including the aerodynamic design considerations and overall performance results
Notes:
Vendor supplied data
Publisher Number:
720711
Access Restriction:
Restricted for use by site license

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