| contributor author | T. J. Sullivan | |
| date accessioned | 2017-05-08T23:33:59Z | |
| date available | 2017-05-08T23:33:59Z | |
| date copyright | October, 1990 | |
| date issued | 1990 | |
| identifier issn | 0889-504X | |
| identifier other | JOTUEI-28606#579_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/107683 | |
| description abstract | The aerodynamic performance of a scale-model, counterrotating unducted fan has been determined and the results are discussed herein. Experimental investigations were conducted using the scale-model propulsor simulator and uniquely shaped fan blades designed by the General Electric Company under contract to NASA. The blades, designed for a high disk loading at Mach 0.72, 35,000 ft altitude max climb condition, are aft-mounted on the simulator in a “pusher” configuration. Data are compared with analytical predictions at the design point and show good agreement. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Aerodynamic Performance of a Scale-Model, Counterrotating Unducted Fan | |
| type | Journal Paper | |
| journal volume | 112 | |
| journal issue | 4 | |
| journal title | Journal of Turbomachinery | |
| identifier doi | 10.1115/1.2927696 | |
| journal fristpage | 579 | |
| journal lastpage | 586 | |
| identifier eissn | 1528-8900 | |
| keywords | Design | |
| keywords | Disks AND Blades | |
| tree | Journal of Turbomachinery:;1990:;volume( 112 ):;issue: 004 | |
| contenttype | Fulltext | |
