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    Influence of Flow Coefficient and Flow Structure on Rotational Cavitation in Inducer

    Source: Journal of Fluids Engineering:;2012:;volume( 134 ):;issue: 002::page 21302
    Author:
    Naoki Tani
    ,
    Yoshinobu Tsujimoto
    ,
    Nobuhiro Yamanishi
    DOI: 10.1115/1.4005903
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Cavitation instability is a major vibration source in turbopump inducers, and its prevention is a critical design problem in rocket-engine development. As reported by Kang et al. , (2009, “Cause of Cavitation Instabilities in Three Dimensional Inducer,” Int. J. Fluid Mach. Syst., 2 (3), pp. 206–214), the flow coefficient plays an important role in the onset of cavitation instabilities such as rotating and asymmetric cavitation. At high flow rates, various cavitation instabilities occur; on the other hand, as the flow coefficient is reduced, these cavitation instabilities either become absent or may change in character. The purpose of the present study is to investigate the relationship between rotating cavitation and flow coefficient through numerical simulations using the Combustion Research Unstructured Navier-stokes solver with CHemistry (CRUNCH) computational fluid dynamics (CFD) code (Ahuja et al. , 2001, “Simulations of Cavitating Flows Using Hybrid Unstructured Meshes,” J. Fluids Eng.Trans ASME, 123 (2), pp. 331–340), and to investigate the internal flow. As a first step, the interaction between the tip vortex and inducer blade was investigated through steady-state simulations. The tip vortex was identified by a vortex detection variable, i.e., the Q-function, a second invariant of the velocity tensor, and the distance between the blade and Q-function peak was measured. For a better understanding of cavitation instabilities, unsteady simulations were also performed for two different flow coefficients. The internal flow was carefully investigated, and the relation between cavity collapse/growth and the change in angle of attack was evaluated. The tip-vortex interaction is not a primary cause of unsteady cavitation, but the negative flow divergence caused by cavity collapse has a great influence on the flow angle. Moreover, changes in flow angle also introduce backflow from the tip clearance; these two factors are primary causes of cavitation instability. When the flow coefficient is large, the backflow is weak, and the interaction with the cavity collapse is strong. In contrast, as the flow coefficient decreases, stronger backflow occurs, and the interaction between backflow, cavity collapse, and flow angle weakens.
    keyword(s): Computational fluid dynamics , Engineering simulation , Blades , Cavities , Flow (Dynamics) , Cavitation , Force , Steady state AND Wake turbulence ,
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      Influence of Flow Coefficient and Flow Structure on Rotational Cavitation in Inducer

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    http://yetl.yabesh.ir/yetl1/handle/yetl/149185
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    • Journal of Fluids Engineering

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    contributor authorNaoki Tani
    contributor authorYoshinobu Tsujimoto
    contributor authorNobuhiro Yamanishi
    date accessioned2017-05-09T00:51:30Z
    date available2017-05-09T00:51:30Z
    date copyrightFebruary, 2012
    date issued2012
    identifier issn0098-2202
    identifier otherJFEGA4-27518#021302_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/149185
    description abstractCavitation instability is a major vibration source in turbopump inducers, and its prevention is a critical design problem in rocket-engine development. As reported by Kang et al. , (2009, “Cause of Cavitation Instabilities in Three Dimensional Inducer,” Int. J. Fluid Mach. Syst., 2 (3), pp. 206–214), the flow coefficient plays an important role in the onset of cavitation instabilities such as rotating and asymmetric cavitation. At high flow rates, various cavitation instabilities occur; on the other hand, as the flow coefficient is reduced, these cavitation instabilities either become absent or may change in character. The purpose of the present study is to investigate the relationship between rotating cavitation and flow coefficient through numerical simulations using the Combustion Research Unstructured Navier-stokes solver with CHemistry (CRUNCH) computational fluid dynamics (CFD) code (Ahuja et al. , 2001, “Simulations of Cavitating Flows Using Hybrid Unstructured Meshes,” J. Fluids Eng.Trans ASME, 123 (2), pp. 331–340), and to investigate the internal flow. As a first step, the interaction between the tip vortex and inducer blade was investigated through steady-state simulations. The tip vortex was identified by a vortex detection variable, i.e., the Q-function, a second invariant of the velocity tensor, and the distance between the blade and Q-function peak was measured. For a better understanding of cavitation instabilities, unsteady simulations were also performed for two different flow coefficients. The internal flow was carefully investigated, and the relation between cavity collapse/growth and the change in angle of attack was evaluated. The tip-vortex interaction is not a primary cause of unsteady cavitation, but the negative flow divergence caused by cavity collapse has a great influence on the flow angle. Moreover, changes in flow angle also introduce backflow from the tip clearance; these two factors are primary causes of cavitation instability. When the flow coefficient is large, the backflow is weak, and the interaction with the cavity collapse is strong. In contrast, as the flow coefficient decreases, stronger backflow occurs, and the interaction between backflow, cavity collapse, and flow angle weakens.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleInfluence of Flow Coefficient and Flow Structure on Rotational Cavitation in Inducer
    typeJournal Paper
    journal volume134
    journal issue2
    journal titleJournal of Fluids Engineering
    identifier doi10.1115/1.4005903
    journal fristpage21302
    identifier eissn1528-901X
    keywordsComputational fluid dynamics
    keywordsEngineering simulation
    keywordsBlades
    keywordsCavities
    keywordsFlow (Dynamics)
    keywordsCavitation
    keywordsForce
    keywordsSteady state AND Wake turbulence
    treeJournal of Fluids Engineering:;2012:;volume( 134 ):;issue: 002
    contenttypeFulltext
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