| contributor author | N. O. Stockman | |
| contributor author | S. Lieblein | |
| contributor author | I. J. Loeffler | |
| date accessioned | 2017-05-09T01:36:20Z | |
| date available | 2017-05-09T01:36:20Z | |
| date copyright | October, 1973 | |
| date issued | 1973 | |
| identifier issn | 1528-8919 | |
| identifier other | JETPEZ-25381#293_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/163745 | |
| description abstract | Results are presented for a wind tunnel investigation of three single VTOL lift fan stages designed for the same overall total pressure ratio at different rotor tip speeds. The stages were tested in a model lift fan installed in a wing pod. The three stages had essentially the same aerodynamic performance along the operating line. However, differences in stage thrust characteristics were obtained when a variation in back pressure was imposed on the stages by crossflow effects and thrust-vectoring louvers. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Effect of Rotor Design Tip Speed on Aerodynamic Performance of a Model VTOL Lift Fan Under Static and Crossflow Conditions | |
| type | Journal Paper | |
| journal volume | 95 | |
| journal issue | 4 | |
| journal title | Journal of Engineering for Gas Turbines and Power | |
| identifier doi | 10.1115/1.3445735 | |
| journal fristpage | 293 | |
| journal lastpage | 300 | |
| identifier eissn | 0742-4795 | |
| keywords | Design | |
| keywords | Rotors | |
| keywords | Pressure | |
| keywords | Thrust | |
| keywords | Wind tunnels AND Wings | |
| tree | Journal of Engineering for Gas Turbines and Power:;1973:;volume( 095 ):;issue: 004 | |
| contenttype | Fulltext | |