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    Hypersonic Rarefied Viscous Interaction Over a Semi-Infinite Flat Plate

    Source: Journal of Applied Mechanics:;1973:;volume( 040 ):;issue: 004::page 857
    Author:
    K. E. Kasza
    ,
    W. L. Chow
    DOI: 10.1115/1.3423175
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The problem of hypersonic rarefied viscous interaction over a semi-infinite flat plate has been solved using Meksyn’s asymptotic method of integrating the full nonsimilar boundary-layer equations. The primary phenomena of “incomplete compression”, velocity slip, and temperature jump are incorporated into the analysis. Results are obtained for induced wall pressure, skin friction, and Stanton number variation along the plate. Detailed results are also obtained for developing velocity profiles and shock location. The pressure plateau within the merged layer region is correctly predicted and the solutions merge far downstream with the strong interaction solutions where rarefied gas effects become negligible.
    keyword(s): Flat plates , Pressure , Temperature , Skin friction (Fluid dynamics) , Shock (Mechanics) , Boundary layers , Compression AND Equations ,
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      Hypersonic Rarefied Viscous Interaction Over a Semi-Infinite Flat Plate

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    http://yetl.yabesh.ir/yetl1/handle/yetl/163326
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    contributor authorK. E. Kasza
    contributor authorW. L. Chow
    date accessioned2017-05-09T01:35:36Z
    date available2017-05-09T01:35:36Z
    date copyrightDecember, 1973
    date issued1973
    identifier issn0021-8936
    identifier otherJAMCAV-25994#857_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/163326
    description abstractThe problem of hypersonic rarefied viscous interaction over a semi-infinite flat plate has been solved using Meksyn’s asymptotic method of integrating the full nonsimilar boundary-layer equations. The primary phenomena of “incomplete compression”, velocity slip, and temperature jump are incorporated into the analysis. Results are obtained for induced wall pressure, skin friction, and Stanton number variation along the plate. Detailed results are also obtained for developing velocity profiles and shock location. The pressure plateau within the merged layer region is correctly predicted and the solutions merge far downstream with the strong interaction solutions where rarefied gas effects become negligible.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleHypersonic Rarefied Viscous Interaction Over a Semi-Infinite Flat Plate
    typeJournal Paper
    journal volume40
    journal issue4
    journal titleJournal of Applied Mechanics
    identifier doi10.1115/1.3423175
    journal fristpage857
    journal lastpage862
    identifier eissn1528-9036
    keywordsFlat plates
    keywordsPressure
    keywordsTemperature
    keywordsSkin friction (Fluid dynamics)
    keywordsShock (Mechanics)
    keywordsBoundary layers
    keywordsCompression AND Equations
    treeJournal of Applied Mechanics:;1973:;volume( 040 ):;issue: 004
    contenttypeFulltext
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