| contributor author | S. R. Manwaring | |
| contributor author | S. Fleeter | |
| date accessioned | 2017-05-08T23:42:58Z | |
| date available | 2017-05-08T23:42:58Z | |
| date copyright | January, 1993 | |
| date issued | 1993 | |
| identifier issn | 0889-504X | |
| identifier other | JOTUEI-28627#197_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/112864 | |
| description abstract | A series of experiments is performed in an extensively instrumented axial flow research compressor to investigate the fundamental flow physics of wake-generated periodic rotor blade row unsteady aerodynamics at realistic values of the reduced frequency. Unique unsteady data are obtained that describe the fundamental unsteady aerodynamic gust interaction phenomena on the first-stage rotor blades of a research axial flow compressor generated by the wakes from the inlet guide vanes. In these experiments, the effects of steady blade aerodynamic loading and the aerodynamic forcing function, including both the transverse and chordwise gust components, and the amplitude of the gusts, are investigated and quantified. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Rotor Blade Unsteady Aerodynamic Gust Response to Inlet Guide Vane Wakes | |
| type | Journal Paper | |
| journal volume | 115 | |
| journal issue | 1 | |
| journal title | Journal of Turbomachinery | |
| identifier doi | 10.1115/1.2929207 | |
| journal fristpage | 197 | |
| journal lastpage | 206 | |
| identifier eissn | 1528-8900 | |
| keywords | Wakes | |
| keywords | Rotors | |
| keywords | Blades | |
| keywords | Axial flow | |
| keywords | Physics | |
| keywords | Flow (Dynamics) | |
| keywords | Aerodynamics AND Compressors | |
| tree | Journal of Turbomachinery:;1993:;volume( 115 ):;issue: 001 | |
| contenttype | Fulltext | |
