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    On Turbulence Measurements and Analyses in a Two-Stage Two-Spool Turbine Rig

    Source: Journal of Turbomachinery:;2017:;volume( 139 ):;issue: 007::page 71008
    Author:
    Bauinger, Sabine
    ,
    Behre, Stephan
    ,
    Lengani, Davide
    ,
    Guendogdu, Yavuz
    ,
    Heitmeir, Franz
    ,
    Goettlich, Emil
    DOI: 10.1115/1.4035508
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Since the experiment in turbulence research is of very high importance for evaluating turbulence hypothesis, turbulence measurements were carried out in a two-stage two-spool transonic turbine test rig at the Institute for Thermal Turbomachinery and Machine Dynamics in Graz in which the two rotors are counter-rotating with two different rotational speeds. For the current measurement campaign, triple hot-wire probes, which represent a very new measurement technique in this test rig, were used and their results validated with a fast response aerodynamic pressure probe (FRAPP). Based on the data measured with this device, turbulence intensities may be determined using a method called Fourier filtering. If the classical ensemble averaging procedure with only one trigger is applied, the periodic fluctuations of the other rotor will artificially increase the stochastic fluctuations. Therefore, the two trigger signals of the two rotors require a special analysis method, which was established at Graz University of Technology. The results from this method will be compared to the classical triple decomposition, which uses only one trigger signal. With this analysis tool, it is not only possible to evaluate unsteady signals triggered by one of the two rotors, but also the unsteady interactions of the rotors can be determined and investigated.
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      On Turbulence Measurements and Analyses in a Two-Stage Two-Spool Turbine Rig

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    contributor authorBauinger, Sabine
    contributor authorBehre, Stephan
    contributor authorLengani, Davide
    contributor authorGuendogdu, Yavuz
    contributor authorHeitmeir, Franz
    contributor authorGoettlich, Emil
    date accessioned2017-11-25T07:19:53Z
    date available2017-11-25T07:19:53Z
    date copyright2017/7/3
    date issued2017
    identifier issn0889-504X
    identifier otherturbo_139_07_071008.pdf
    identifier urihttp://138.201.223.254:8080/yetl1/handle/yetl/4236082
    description abstractSince the experiment in turbulence research is of very high importance for evaluating turbulence hypothesis, turbulence measurements were carried out in a two-stage two-spool transonic turbine test rig at the Institute for Thermal Turbomachinery and Machine Dynamics in Graz in which the two rotors are counter-rotating with two different rotational speeds. For the current measurement campaign, triple hot-wire probes, which represent a very new measurement technique in this test rig, were used and their results validated with a fast response aerodynamic pressure probe (FRAPP). Based on the data measured with this device, turbulence intensities may be determined using a method called Fourier filtering. If the classical ensemble averaging procedure with only one trigger is applied, the periodic fluctuations of the other rotor will artificially increase the stochastic fluctuations. Therefore, the two trigger signals of the two rotors require a special analysis method, which was established at Graz University of Technology. The results from this method will be compared to the classical triple decomposition, which uses only one trigger signal. With this analysis tool, it is not only possible to evaluate unsteady signals triggered by one of the two rotors, but also the unsteady interactions of the rotors can be determined and investigated.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleOn Turbulence Measurements and Analyses in a Two-Stage Two-Spool Turbine Rig
    typeJournal Paper
    journal volume139
    journal issue7
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.4035508
    journal fristpage71008
    journal lastpage071008-11
    treeJournal of Turbomachinery:;2017:;volume( 139 ):;issue: 007
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
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