contributor author | H. S. Wijesinghe | |
contributor author | C. S. Tan | |
contributor author | E. E. Covert | |
date accessioned | 2017-05-09T00:09:02Z | |
date available | 2017-05-09T00:09:02Z | |
date copyright | April, 2002 | |
date issued | 2002 | |
identifier issn | 0889-504X | |
identifier other | JOTUEI-28695#269_1.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/127646 | |
description abstract | A two-dimensional computational study was conducted to characterize the density wake induced force and moment fluctuations on a compressor blade row. The flow simulations indicate unsteady blade excitation generated by: (1) density wake fluid directed to the blade suction surface, (2) axial deflection of the blade passage shock wave position and (3) formation of a separation bubble on the blade suction surface. The blade force and moment fluctuation amplitudes are found to scale with the nondimensional density wake width w/c and a nondimensional density parameter ρ*. | |
publisher | The American Society of Mechanical Engineers (ASME) | |
title | Aerodynamic Response of Turbomachinery Blade Rows to Convecting Density Wakes | |
type | Journal Paper | |
journal volume | 124 | |
journal issue | 2 | |
journal title | Journal of Turbomachinery | |
identifier doi | 10.1115/1.1311287 | |
journal fristpage | 269 | |
journal lastpage | 274 | |
identifier eissn | 1528-8900 | |
keywords | Density | |
keywords | Force | |
keywords | Wakes | |
keywords | Blades | |
keywords | Suction | |
keywords | Fluids | |
keywords | Flow (Dynamics) | |
keywords | Separation (Technology) | |
keywords | Shock waves | |
keywords | Fluctuations (Physics) | |
keywords | Compressors AND Turbomachinery | |
tree | Journal of Turbomachinery:;2002:;volume( 124 ):;issue: 002 | |
contenttype | Fulltext | |