contributor author | Z. W. He | |
contributor author | S. Y. Zhang | |
date accessioned | 2017-05-08T23:22:26Z | |
date available | 2017-05-08T23:22:26Z | |
date copyright | July, 1986 | |
date issued | 1986 | |
identifier issn | 1528-8919 | |
identifier other | JETPEZ-26637#562_1.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/101113 | |
description abstract | It is found experimentally that blowing at the lip separation of an inlet obviously reduces the turbulence at the inlet exit, and apparently reduces the intensity of pressure fluctuations caused by the shock-boundary layer interaction downstream of the throat. The coherence between pressure in the interaction region and total pressure at the exit is also reduced. The coherence between the pressure in the lip separation region and total pressure at the exit is 0.32. If, in addition, there is a stronger shock downstream of the throat, the abovementioned coherence is reduced to 0.06. | |
publisher | The American Society of Mechanical Engineers (ASME) | |
title | Lip Separate Flow Blowing and Analysis of Coherence of Inlet | |
type | Journal Paper | |
journal volume | 108 | |
journal issue | 3 | |
journal title | Journal of Engineering for Gas Turbines and Power | |
identifier doi | 10.1115/1.3239947 | |
journal fristpage | 562 | |
journal lastpage | 565 | |
identifier eissn | 0742-4795 | |
keywords | Pressure | |
keywords | Flow (Dynamics) | |
keywords | Separation (Technology) | |
keywords | Turbulence | |
keywords | Fluctuations (Physics) AND Shock (Mechanics) | |
tree | Journal of Engineering for Gas Turbines and Power:;1986:;volume( 108 ):;issue: 003 | |
contenttype | Fulltext | |