Design and analysis of axial aspirated compressor stages
Thesis (Ph.D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1999. === Includes bibliographical references (p. 145-150). === The pressure ratio of axial compressor stages can be significantly increased by controlling the development of blade and endwall boundary laye...
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| Format: | Others |
| Language: | English |
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Massachusetts Institute of Technology
2005
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| Online Access: | http://hdl.handle.net/1721.1/9362 |