Report of tests of a compressor configuration of CD blading
| dc.contributor.advisor | Shreeve, Raymond P. | |
| dc.contributor.author | Koyuncu, Yuksel | |
| dc.date | March 1984 | |
| dc.date.accessioned | 2012-11-19T23:51:15Z | |
| dc.date.available | 2012-11-19T23:51:15Z | |
| dc.date.issued | 1984-03 | |
| dc.identifier.uri | https://hdl.handle.net/10945/19530 | |
| dc.description.abstract | Results of 14 tests in a subsonic cascade are reported in which the air inlet angle and Reynolds number were varied. The cascade contained 20 Controlled Diffusion (CD) blades , with 5.01 inches chord, aspect ratio of 2.0 and solidity of 1.67. Pneumatic probe surveys and surface pressure measurements were used to obtain blade performance and flow quality data. There was no measurable influence of the Reynolds number on the blade losses in the range of Re. = 474000 to Re. = 690000. Fourteen tests, using seven different inlet air angles over a range of 24 to 46 degrees generated generally well behaved blade performance parameters. The results were compared with previous results from a corresponding cascade of DCA blades. | |
| dc.description.uri | http://archive.org/details/reportoftestsofc1094519530 | |
| dc.language.iso | en_US | |
| dc.publisher | Monterey, California. Naval Postgraduate School | en_US |
| dc.rights | Copyright is reserved by the copyright owner | |
| dc.subject.lcsh | Aeronautics | en_US |
| dc.title | Report of tests of a compressor configuration of CD blading | en_US |
| dc.type | Thesis | en_US |
| dc.contributor.corporate | Naval Postgraduate School (U.S.) | |
| dc.contributor.department | Aeronautics | |
| dc.subject.author | Cascade | en_US |
| dc.subject.author | CD cascade | en_US |
| dc.description.service | First Lieutenant, Turkish Air Force | |
| etd.thesisdegree.name | M.S. in Aeronautical Engineering | en_US |
| etd.thesisdegree.level | Masters | en_US |
| etd.thesisdegree.discipline | Aeronautical Engineering | en_US |
| etd.thesisdegree.grantor | Naval Postgraduate School | en_US |
| dc.description.distributionstatement | Approved for public release; distribution is unlimited. |
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