Test of Supersonic Compressor Cascade with Splitter Vanes and Vortex Generators on Blades
The report describes experimental research conducted with a linear, stationary, supersonic compressor cascade with blades of constant spanwise geometry and contoured sidewalls. The cascade incorporated splitter vanes midway between blades in the latter half of each blade passage. The influence of sp...
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| Format: | Book |
| Language: | English |
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Ft. Belvoir
Defense Technical Information Center
NOV 1973
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