Design and tests of a six-stage axial-flow compressor having a tip speed of 550 feet per second and a flat operating characteristic at constant speed
A six-stage axial-flow compressor with a 550 feet per second tip speed and a flat operating characteristic (constant stagnation-pressure ratio at constant speed over the operating range of the compressor) was designed and tested. The design theory and test results are presented in this thesis. It wa...
Main Author: | Maynard, John W. Jr |
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Other Authors: | Aeronautical Engineering |
Format: | Others |
Language: | en_US |
Published: |
Virginia Polytechnic Institute
2018
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Subjects: | |
Online Access: | http://hdl.handle.net/10919/82620 |
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