| contributor author | Ghassan Khabbaz | |
| contributor author | Yasutoshi Senoo | |
| date accessioned | 2017-05-09T01:35:49Z | |
| date available | 2017-05-09T01:35:49Z | |
| date copyright | September, 1961 | |
| date issued | 1961 | |
| identifier issn | 0098-2202 | |
| identifier other | JFEGA4-27232#371_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/163419 | |
| description abstract | An experimental study of the influence of tip clearance on the stall limits of compressor blades was conducted on a rectilinear cascade. By using the mirror and image technique the end wall boundary layer near the clearance was dispensed with. The blade loading was maximum at a distance from the tip clearance, but the clearance was found to relieve the pressure gradient in general and to retard stalling. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | The Influence of Tip Clearance on Stall Limits of a Rectilinear Cascade of Compressor Blades | |
| type | Journal Paper | |
| journal volume | 83 | |
| journal issue | 3 | |
| journal title | Journal of Fluids Engineering | |
| identifier doi | 10.1115/1.3658967 | |
| journal fristpage | 371 | |
| journal lastpage | 377 | |
| identifier eissn | 1528-901X | |
| keywords | Compressors | |
| keywords | Cascades (Fluid dynamics) | |
| keywords | Clearances (Engineering) | |
| keywords | Blades | |
| keywords | Mirrors | |
| keywords | Pressure gradient AND Boundary layers | |
| tree | Journal of Fluids Engineering:;1961:;volume( 083 ):;issue: 003 | |
| contenttype | Fulltext | |
