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    Effect of Suction on the Stability of Supersonic Boundary Layers. Part I—Second-Mode Waves

    Source: Journal of Fluids Engineering:;1991:;volume( 113 ):;issue: 004::page 591
    Author:
    A. A. Al-Maaitah
    ,
    A. H. Nayfeh
    ,
    J. A. Masad
    DOI: 10.1115/1.2926520
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The effect of suction on the second (Mack) mode of instability in supersonic and hypersonic two-dimensional boundary layers is investigated. The results show that suction has a stabilizing effect on these waves; it reduces the peak amplification and shifts it toward a higher frequency. In the presence of suction, the most amplified Mack mode remains two-dimensional. The effectiveness of suction in stabilizing Mack waves decreases as the Mach number increases. Variations of the growth rates of the most amplified Mack mode and the corresponding frequencies and wave numbers with mass flux are found to be almost linear. The frequencies and wave numbers corresponding to the most amplified Mack mode increase by increasing the suction level.
    keyword(s): Suction , Waves , Boundary layers , Stability , Frequency AND Mach number ,
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      Effect of Suction on the Stability of Supersonic Boundary Layers. Part I—Second-Mode Waves

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/108674
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    • Journal of Fluids Engineering

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    contributor authorA. A. Al-Maaitah
    contributor authorA. H. Nayfeh
    contributor authorJ. A. Masad
    date accessioned2017-05-08T23:35:45Z
    date available2017-05-08T23:35:45Z
    date copyrightDecember, 1991
    date issued1991
    identifier issn0098-2202
    identifier otherJFEGA4-27062#591_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/108674
    description abstractThe effect of suction on the second (Mack) mode of instability in supersonic and hypersonic two-dimensional boundary layers is investigated. The results show that suction has a stabilizing effect on these waves; it reduces the peak amplification and shifts it toward a higher frequency. In the presence of suction, the most amplified Mack mode remains two-dimensional. The effectiveness of suction in stabilizing Mack waves decreases as the Mach number increases. Variations of the growth rates of the most amplified Mack mode and the corresponding frequencies and wave numbers with mass flux are found to be almost linear. The frequencies and wave numbers corresponding to the most amplified Mack mode increase by increasing the suction level.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleEffect of Suction on the Stability of Supersonic Boundary Layers. Part I—Second-Mode Waves
    typeJournal Paper
    journal volume113
    journal issue4
    journal titleJournal of Fluids Engineering
    identifier doi10.1115/1.2926520
    journal fristpage591
    journal lastpage597
    identifier eissn1528-901X
    keywordsSuction
    keywordsWaves
    keywordsBoundary layers
    keywordsStability
    keywordsFrequency AND Mach number
    treeJournal of Fluids Engineering:;1991:;volume( 113 ):;issue: 004
    contenttypeFulltext
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