2 edition of Performance of single-stage axial-flow transonic compressor with rotor and stator aspect ratios of 1.19 and 1.26, respectively, and with design pressure ratio of 2.05 found in the catalog.
Performance of single-stage axial-flow transonic compressor with rotor and stator aspect ratios of 1.19 and 1.26, respectively, and with design pressure ratio of 2.05
Royce D Moore
1978 by National Aeronautics and Space Administration, Scientific and Technical Information Office, For sale by the National Technical Information Service] in Washington, D.C, [Springfield, Va .
Written in English
|Statement||Royce D. Moore and Lonnie Reid|
|Series||NASA technical paper -- 1659|
|Contributions||Reid, Lonnie, Lewis Research Center, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office|
|The Physical Object|
|Pagination||i, 101 p. :|
|Number of Pages||101|
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