| dc.contributor.author | Kubota, Shigeo | en_US |
| dc.contributor.other | Massachusetts Institute of Technology. Gas Turbine Laboratory | en_US |
| dc.date.accessioned | 2016-10-06T21:22:08Z | |
| dc.date.available | 2016-10-06T21:22:08Z | |
| dc.date.issued | 1959 | en_US |
| dc.identifier.uri | http://hdl.handle.net/1721.1/104716 | |
| dc.description | September 1959 | en_US |
| dc.description | Includes bibliographical references (page 27) | en_US |
| dc.description.abstract | A theoretical method to estimate the effect of axial velocity change through a cascade was investigated. The change of axial velocity was reproduced by distributing sinks and sources within the blade passages, and the conclusions are set forth in some simple formulae. Some graphs for the numerical evaluation of the performance of NACA 65 series cascades were prepared, and several examples were compared with experimental data. | en_US |
| dc.description.sponsorship | Under the sponsorship of: General Electric Company, Allison Division of General Motors Corporation and Westinghouse Electric Corporation | en_US |
| dc.format.extent | [40] pages (some unnumbered) | en_US |
| dc.publisher | Cambridge, Mass. : Gas Turbine Laboratory, Massachusetts Institute of Technology, [1959] | en_US |
| dc.relation.ispartofseries | GTL report #56 | en_US |
| dc.subject.lcc | TJ778.M41 G24 no.56 | en_US |
| dc.subject.lcsh | Aerofoils | en_US |
| dc.title | Cascade performance with accelerated or decelerated axial velocity | en_US |
| dc.type | Technical Report | en_US |
| dc.identifier.oclc | 14200332 | en_US |
