| dc.contributor.author | Khabbaz, Ghassan R. (Ghassan Raji) | en_US |
| dc.contributor.other | Massachusetts Institute of Technology. Gas Turbine Laboratory | en_US |
| dc.date.accessioned | 2016-10-06T21:21:52Z | |
| dc.date.available | 2016-10-06T21:21:52Z | |
| dc.date.issued | 1959 | en_US |
| dc.identifier.uri | http://hdl.handle.net/1721.1/104673 | |
| dc.description | August 1959 | en_US |
| dc.description | Also issued as: Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 1959 | en_US |
| dc.description | Includes bibliographical references (leaves 20-21) | en_US |
| dc.description.abstract | An experimental study of the influence of tip clearance on the stall limits of compressor blades was conducted on a two dimensional rectilinear cascade. By using the mirror and image technique the end wall boundary layer in the gap was dispensed with. The clearance was found to relieve the pressure gradient and to retard stalling. The loading on the blade near the slot was found to be higher than that at a distance further along. | en_US |
| dc.description.sponsorship | Under the sponsorship of: General Electric Company, Allison Division of General Motors and Corporation Westinghouse Electric Corporation | en_US |
| dc.format.extent | 21, [27] leaves | en_US |
| dc.publisher | Cambridge, Mass. : Gas Turbine Laboratory, Massachusetts Institute of Technology, [1959] | en_US |
| dc.relation.ispartofseries | GTL report #54 | en_US |
| dc.subject.lcc | TJ267.A1 M37 no.54 | en_US |
| dc.subject.lcsh | Cascades (Fluid dynamics) | en_US |
| dc.subject.lcsh | Compressors -- Blades | en_US |
| dc.subject.lcsh | Aerodynamic load | en_US |
| dc.title | The influence of tip clearance on stall limits of a rectilinear cascade of compressor blades | en_US |
| dc.type | Technical Report | en_US |
| dc.identifier.oclc | 09162414 | en_US |
