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    The Effects of Turbulence Stimulators on Cavitation Inception of Axisymmetric Headforms

    Source: Journal of Fluids Engineering:;1986:;volume( 108 ):;issue: 002::page 261
    Author:
    T. T. Huang
    DOI: 10.1115/1.3242573
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Cavitation inception observations were made in the DTNSRDC 36-inch water tunnel on three axisymmetric headforms with and without various turbulence stimulators installed. Direct transition measurements, made on two of the headforms with and without distributed surface roughness, were found to correlate reasonably well with the computed spatial amplification factors, eN , at the separation locations. The computed eN factors were then used to estimate transition at other test conditions (without direct transition measurements). The predicted transition locations on all three smooth headforms occur at positions considerably aft of the minimum pressure locations. The three smooth headforms have different types of incipient cavitation—small band, transient spot, traveling bubble, and attached spot. The measured cavitation inception numbers for those cases are all significantly smaller than the computed negative values of the minimum pressure coefficient, −Cpmin . The predicted transition locations on the three headforms with densely and loosely packed 60-μm distributed roughness occur at a considerable distance upstream of the minimum pressure locations. Therefore, the flows over all three headforms with distributed roughness are turbulent at the Cpmin locations for the Reynolds numbers tested. Under this condition, the measured cavitation inception numbers are found to approximate well with the values of −Cpmin . The incipient cavitation is in the form of attached small bubble lines evenly distributed around the minimum pressure locations. The measured cavitation inception numbers for the three headforms with an isolated roughness band located upstream of the minimum pressure locations are found to approximate the computed values of −Cpmin when the roughness Reynolds number (Rk = uk K/ν) is equal to 600 and to be smaller than the values of −Cpmin when the value of Rk is less than 600. The incipient cavitation observed is attached patch type cavitation occurring in the vicinity of the minimum pressure location. The uncertainty of the measured cavitation inception numbers, in terms of the maximum deviations form the mean values of repeated measurements, is generally less than 0.02.
    keyword(s): Turbulence , Cavitation , Pressure , Surface roughness , Measurement , Reynolds number , Bubbles , Water tunnels , Travel , Uncertainty , Flow (Dynamics) AND Separation (Technology) ,
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      The Effects of Turbulence Stimulators on Cavitation Inception of Axisymmetric Headforms

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    http://yetl.yabesh.ir/yetl1/handle/yetl/101326
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    contributor authorT. T. Huang
    date accessioned2017-05-08T23:22:49Z
    date available2017-05-08T23:22:49Z
    date copyrightJune, 1986
    date issued1986
    identifier issn0098-2202
    identifier otherJFEGA4-27020#261_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/101326
    description abstractCavitation inception observations were made in the DTNSRDC 36-inch water tunnel on three axisymmetric headforms with and without various turbulence stimulators installed. Direct transition measurements, made on two of the headforms with and without distributed surface roughness, were found to correlate reasonably well with the computed spatial amplification factors, eN , at the separation locations. The computed eN factors were then used to estimate transition at other test conditions (without direct transition measurements). The predicted transition locations on all three smooth headforms occur at positions considerably aft of the minimum pressure locations. The three smooth headforms have different types of incipient cavitation—small band, transient spot, traveling bubble, and attached spot. The measured cavitation inception numbers for those cases are all significantly smaller than the computed negative values of the minimum pressure coefficient, −Cpmin . The predicted transition locations on the three headforms with densely and loosely packed 60-μm distributed roughness occur at a considerable distance upstream of the minimum pressure locations. Therefore, the flows over all three headforms with distributed roughness are turbulent at the Cpmin locations for the Reynolds numbers tested. Under this condition, the measured cavitation inception numbers are found to approximate well with the values of −Cpmin . The incipient cavitation is in the form of attached small bubble lines evenly distributed around the minimum pressure locations. The measured cavitation inception numbers for the three headforms with an isolated roughness band located upstream of the minimum pressure locations are found to approximate the computed values of −Cpmin when the roughness Reynolds number (Rk = uk K/ν) is equal to 600 and to be smaller than the values of −Cpmin when the value of Rk is less than 600. The incipient cavitation observed is attached patch type cavitation occurring in the vicinity of the minimum pressure location. The uncertainty of the measured cavitation inception numbers, in terms of the maximum deviations form the mean values of repeated measurements, is generally less than 0.02.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleThe Effects of Turbulence Stimulators on Cavitation Inception of Axisymmetric Headforms
    typeJournal Paper
    journal volume108
    journal issue2
    journal titleJournal of Fluids Engineering
    identifier doi10.1115/1.3242573
    journal fristpage261
    journal lastpage268
    identifier eissn1528-901X
    keywordsTurbulence
    keywordsCavitation
    keywordsPressure
    keywordsSurface roughness
    keywordsMeasurement
    keywordsReynolds number
    keywordsBubbles
    keywordsWater tunnels
    keywordsTravel
    keywordsUncertainty
    keywordsFlow (Dynamics) AND Separation (Technology)
    treeJournal of Fluids Engineering:;1986:;volume( 108 ):;issue: 002
    contenttypeFulltext
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