| contributor author | Karl Kovach | |
| contributor author | D. M. Sandercock | |
| date accessioned | 2017-05-09T01:08:47Z | |
| date available | 2017-05-09T01:08:47Z | |
| date copyright | July, 1961 | |
| date issued | 1961 | |
| identifier issn | 1528-8919 | |
| identifier other | JETPEZ-26617#303_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/155056 | |
| description abstract | A five-stage axial-flow compressor with all rotors operating with transonic relative inlet Mach numbers was designed as a research vehicle at the Lewis Research Center in 1952. The compressor was designed and tested as a component of a turbojet engine. This paper summarizes the research work done on this compressor including the aerodynamic design and detailed performance characteristics. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Aerodynamic Design and Performance of Five-Stage Transonic Axial-Flow Compressor | |
| type | Journal Paper | |
| journal volume | 83 | |
| journal issue | 3 | |
| journal title | Journal of Engineering for Gas Turbines and Power | |
| identifier doi | 10.1115/1.3673192 | |
| journal fristpage | 303 | |
| journal lastpage | 320 | |
| identifier eissn | 0742-4795 | |
| keywords | Compressors | |
| keywords | Design | |
| keywords | Axial flow | |
| keywords | Turbojets | |
| keywords | Performance characterization | |
| keywords | Mach number | |
| keywords | Engines | |
| keywords | Rotors AND Vehicles | |
| tree | Journal of Engineering for Gas Turbines and Power:;1961:;volume( 083 ):;issue: 003 | |
| contenttype | Fulltext | |