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    Dynamics of Large Buoyant Clouds Generated by Rocket Launches

    Source: Journal of Fluids Engineering:;1972:;volume( 094 ):;issue: 001::page 53
    Author:
    W. S. Hart
    DOI: 10.1115/1.3425385
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Motion pictures of launches of Titan III solid rocket motors were used, in conjunction with conservation equations and knowledge of rocket plume properties, to determine the initial temperature and mass of the large cloud that is generated during these launches. These initial conditions were applied to a mathematical model which accounted for buoyancy, drag and entrainment. The model predicted the radius, altitude, temperature and mass of the cloud as a function of time. The results showed fair agreement with size and altitude data extracted from the movies. This methodology was applied with limited success to smaller scale rocket clouds generated at test stands. The model was also used to predict the behavior of large exhaust clouds under various external temperature profiles. There is some experimental evidence that the model correctly accounts for unstable profiles, and the predictions of cloud rise during inversion conditions agree with what intuition would predict.
    keyword(s): Dynamics (Mechanics) , Rockets , Temperature , Motion , Motors , Drag (Fluid dynamics) , Plumes (Fluid dynamics) , Equations , Exhaust systems , Temperature profiles AND Buoyancy ,
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      Dynamics of Large Buoyant Clouds Generated by Rocket Launches

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    https://yetl.yabesh.ir/yetl1/handle/yetl/162889
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    contributor authorW. S. Hart
    date accessioned2017-05-09T01:34:38Z
    date available2017-05-09T01:34:38Z
    date copyrightMarch, 1972
    date issued1972
    identifier issn0098-2202
    identifier otherJFEGA4-27389#53_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/162889
    description abstractMotion pictures of launches of Titan III solid rocket motors were used, in conjunction with conservation equations and knowledge of rocket plume properties, to determine the initial temperature and mass of the large cloud that is generated during these launches. These initial conditions were applied to a mathematical model which accounted for buoyancy, drag and entrainment. The model predicted the radius, altitude, temperature and mass of the cloud as a function of time. The results showed fair agreement with size and altitude data extracted from the movies. This methodology was applied with limited success to smaller scale rocket clouds generated at test stands. The model was also used to predict the behavior of large exhaust clouds under various external temperature profiles. There is some experimental evidence that the model correctly accounts for unstable profiles, and the predictions of cloud rise during inversion conditions agree with what intuition would predict.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleDynamics of Large Buoyant Clouds Generated by Rocket Launches
    typeJournal Paper
    journal volume94
    journal issue1
    journal titleJournal of Fluids Engineering
    identifier doi10.1115/1.3425385
    journal fristpage53
    journal lastpage60
    identifier eissn1528-901X
    keywordsDynamics (Mechanics)
    keywordsRockets
    keywordsTemperature
    keywordsMotion
    keywordsMotors
    keywordsDrag (Fluid dynamics)
    keywordsPlumes (Fluid dynamics)
    keywordsEquations
    keywordsExhaust systems
    keywordsTemperature profiles AND Buoyancy
    treeJournal of Fluids Engineering:;1972:;volume( 094 ):;issue: 001
    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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