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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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