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    Continuous Monitoring of Binary Gas Mixture Concentration With Application to Turbine Blade Cooling Experiments

    Source: Journal of Turbomachinery:;2000:;volume( 122 ):;issue: 003::page 570
    Author:
    Tomas Strilka
    ,
    Miklos Sajben
    ,
    Professor. Mem. ASME
    ,
    Peter Nagy
    ,
    Associate Professor. Mem. ASME
    DOI: 10.1115/1.1302285
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Turbine blade cooling experiments often use mixtures of air and a heavy gas (CO2, SF6) to simulate coolant/mainstream density ratios. If the mixing of the mainstream with the coolant ejected from the blade is of interest, then it may be necessary to determine the spatial distribution of the heavy gas concentration in the flowfield. Commercial analyzers are too slow and have other disadvantages when used for this purpose. To meet this special need, a device has been developed to monitor the heavy gas concentration continuously in a small sample stream by determining the speed of sound in the sample. Together with the temperature of the sample, the information is sufficient to determine the concentration. The device measures the time of propagation for an ultrasonic burst transverse to the stream. The temperature of the gas contained in the device is controlled and measured. Calibration with several gas mixtures (air and CO2,SF6, He) has shown an uncertainty (Cmeas−Ctrue) of 2 percent over the full concentration range of 0–100 percent for CO2 and SF6. The device is operable in the pressure range from −50 to 100 kPa gage and in the temperature range from 0°C to 40°C. The instrument is rugged and will survive in noisy, turbulent environments. [S0889-504X(00)01202-2]
    keyword(s): Pressure , Flow (Dynamics) , Temperature , Cooling , Speed of sound , Mixtures , Turbine blades , Errors , Gases , Transducers , Calibration , Turbulence , Density , Flowmeters AND Sampling (Acoustical engineering) ,
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      Continuous Monitoring of Binary Gas Mixture Concentration With Application to Turbine Blade Cooling Experiments

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    http://yetl.yabesh.ir/yetl1/handle/yetl/124477
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    • Journal of Turbomachinery

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    contributor authorTomas Strilka
    contributor authorMiklos Sajben
    contributor authorProfessor. Mem. ASME
    contributor authorPeter Nagy
    contributor authorAssociate Professor. Mem. ASME
    date accessioned2017-05-09T00:03:38Z
    date available2017-05-09T00:03:38Z
    date copyrightJuly, 2000
    date issued2000
    identifier issn0889-504X
    identifier otherJOTUEI-28679#570_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/124477
    description abstractTurbine blade cooling experiments often use mixtures of air and a heavy gas (CO2, SF6) to simulate coolant/mainstream density ratios. If the mixing of the mainstream with the coolant ejected from the blade is of interest, then it may be necessary to determine the spatial distribution of the heavy gas concentration in the flowfield. Commercial analyzers are too slow and have other disadvantages when used for this purpose. To meet this special need, a device has been developed to monitor the heavy gas concentration continuously in a small sample stream by determining the speed of sound in the sample. Together with the temperature of the sample, the information is sufficient to determine the concentration. The device measures the time of propagation for an ultrasonic burst transverse to the stream. The temperature of the gas contained in the device is controlled and measured. Calibration with several gas mixtures (air and CO2,SF6, He) has shown an uncertainty (Cmeas−Ctrue) of 2 percent over the full concentration range of 0–100 percent for CO2 and SF6. The device is operable in the pressure range from −50 to 100 kPa gage and in the temperature range from 0°C to 40°C. The instrument is rugged and will survive in noisy, turbulent environments. [S0889-504X(00)01202-2]
    publisherThe American Society of Mechanical Engineers (ASME)
    titleContinuous Monitoring of Binary Gas Mixture Concentration With Application to Turbine Blade Cooling Experiments
    typeJournal Paper
    journal volume122
    journal issue3
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.1302285
    journal fristpage570
    journal lastpage578
    identifier eissn1528-8900
    keywordsPressure
    keywordsFlow (Dynamics)
    keywordsTemperature
    keywordsCooling
    keywordsSpeed of sound
    keywordsMixtures
    keywordsTurbine blades
    keywordsErrors
    keywordsGases
    keywordsTransducers
    keywordsCalibration
    keywordsTurbulence
    keywordsDensity
    keywordsFlowmeters AND Sampling (Acoustical engineering)
    treeJournal of Turbomachinery:;2000:;volume( 122 ):;issue: 003
    contenttypeFulltext
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    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
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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
    yabeshDSpacePersian