Performance of single-stage axial-flow transonic compressor with rotor and stator aspect ratios of 1.63 and 1.77, respectively, and with design pressure ratio of 2.05 /
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| Main Author: | |
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| Corporate Authors: | , |
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| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. : [Springfield, Va.] :
National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service],
1982.
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| Series: | NASA technical paper ;
2001. |
| Subjects: |
Hesburgh Library GovDocs SuDoc Fiche [Lower Level]
| Call Number: |
NAS 1.60:2001
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| Available Request a scan of an article or book chapter |