Thermodynamic Effect on a Cavitating Inducer—Part II: On-Board Measurements of Temperature Depression Within Leading Edge CavitiesSource: Journal of Fluids Engineering:;2010:;volume( 132 ):;issue: 002::page 21304Author:Jean-Pierre Franc
,
Éric Janson
,
Pierre Ramina
,
Guillaume Boitel
,
Michel Riondet
,
Claude Rebattet
DOI: 10.1115/1.4001007Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Temperature depression within the leading edge cavities on a space inducer is measured in Refrigerant 114 using miniature thermocouples mounted on the rotating blades. Time-averaged values of cavity temperature depression are determined all along the descent in cavitation number and correlated with the extent of cavities. In addition to mean values, temperature fluctuations are analyzed with respect to the onset of cavitation instabilities, namely, alternate blade cavitation and supersynchronous rotating cavitation. Temperature spectra relative to a rotating frame of reference are compared with pressure spectra obtained in a fixed frame of reference. Temperature oscillations issued from different blades are compared, and phase shifts between consecutive and opposite blades are evaluated in the case of the supersynchronous instability regime.
keyword(s): Temperature , Cavitation , Blades AND Cavities ,
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contributor author | Jean-Pierre Franc | |
contributor author | Éric Janson | |
contributor author | Pierre Ramina | |
contributor author | Guillaume Boitel | |
contributor author | Michel Riondet | |
contributor author | Claude Rebattet | |
date accessioned | 2017-05-09T00:38:20Z | |
date available | 2017-05-09T00:38:20Z | |
date copyright | February, 2010 | |
date issued | 2010 | |
identifier issn | 0098-2202 | |
identifier other | JFEGA4-27408#021304_1.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/143542 | |
description abstract | Temperature depression within the leading edge cavities on a space inducer is measured in Refrigerant 114 using miniature thermocouples mounted on the rotating blades. Time-averaged values of cavity temperature depression are determined all along the descent in cavitation number and correlated with the extent of cavities. In addition to mean values, temperature fluctuations are analyzed with respect to the onset of cavitation instabilities, namely, alternate blade cavitation and supersynchronous rotating cavitation. Temperature spectra relative to a rotating frame of reference are compared with pressure spectra obtained in a fixed frame of reference. Temperature oscillations issued from different blades are compared, and phase shifts between consecutive and opposite blades are evaluated in the case of the supersynchronous instability regime. | |
publisher | The American Society of Mechanical Engineers (ASME) | |
title | Thermodynamic Effect on a Cavitating Inducer—Part II: On-Board Measurements of Temperature Depression Within Leading Edge Cavities | |
type | Journal Paper | |
journal volume | 132 | |
journal issue | 2 | |
journal title | Journal of Fluids Engineering | |
identifier doi | 10.1115/1.4001007 | |
journal fristpage | 21304 | |
identifier eissn | 1528-901X | |
keywords | Temperature | |
keywords | Cavitation | |
keywords | Blades AND Cavities | |
tree | Journal of Fluids Engineering:;2010:;volume( 132 ):;issue: 002 | |
contenttype | Fulltext |