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Impact of compliant coating on Mack-mode evolution in hypersonic boundary layers
Ji XY(纪晓阳); Dong M(董明); Zhao, Lei
Corresponding AuthorDong, Ming([email protected]) ; Zhao, Lei([email protected])
Source PublicationJOURNAL OF FLUID MECHANICS
2023-10-23
Volume974Pages:32
ISSN0022-1120
AbstractThis paper focuses on the linear evolution of Mack instability modes in a hypersonic boundary layer over a flat plate that is partially coated by a compliant section. The compliant section is a thin, flexible membrane covering on a porous wall consisting of micro holes. The instability pressure could induce a vibration of the membrane, leading to a feedback to the boundary-layer fluids through the transverse velocity fluctuation. Such a process is formulated by an admittance boundary condition for the boundary-layer perturbation, which is dependent on the thickness and tension of the membrane, the properties of the porous wall, and the frequency of the Mack-mode perturbation. Using this admittance condition, the impact of the compliant coating on the Mack growth rate is studied systematically by solving the compressible Orr-Sommerfeld equations. It is found that the compliant coating could suppress the Mack instability with a frequency band in the neighbourhood of the most unstable frequency, and the stabilising frequency band widens as the membrane thickness and tension decrease, indicating a more favourable effect of a softer membrane. For a Mack mode with a specified dimensional frequency - since its dimensionless frequency, normalised by the local boundary-layer thickness and oncoming velocity, increases as it propagates downstream - the second-mode frequency band usually appears in downstream locations, and so does the stabilising effect of the membrane. Thus it is favourable to apply a compliant panel at a downstream region. In this situation, the solid-compliant junction could produce an additional scattering effect on the evolution of the Mack mode due to the sudden change of its boundary condition. The scattering effect is quantified by a transmission coefficient defined by the equivalent amplitude of the compliant-wall perturbation to the solid-wall perturbation, which can be obtained by the harmonic linearised Navier-Stokes (HLNS) approach. If the admittance is weak, then the transmission coefficient can also be predicted by an analytical solution based on the residue theorem. It is found that most of the second modes are suppressed by the scattering effect as long as the argument of the admittance is in the interval [150 degrees, 210 degrees], agreeing with most of the physical situation. The analytical predictions agree well with the HLNS calculations when the modulus of the admittance is less than O(0.1).
Keywordboundary layer stability transition to turbulence
DOI10.1017/jfm.2023.731
Indexed BySCI ; EI
Language英语
WOS IDWOS:001087800700001
WOS KeywordINSTABILITY ; ROUGHNESS ; STABILITY ; RECEPTIVITY ; TRANSITION ; SOUND
WOS Research AreaMechanics ; Physics
WOS SubjectMechanics ; Physics, Fluids & Plasmas
Classification一类/力学重要期刊
Ranking1
ContributorDong, Ming ; Zhao, Lei
Citation statistics
Cited Times:2[WOS]   [WOS Record]     [Related Records in WOS]
Document Type期刊论文
Identifierhttp://dspace.imech.ac.cn/handle/311007/93244
Collection非线性力学国家重点实验室
Recommended Citation
GB/T 7714
Ji XY,Dong M,Zhao, Lei. Impact of compliant coating on Mack-mode evolution in hypersonic boundary layers[J]. JOURNAL OF FLUID MECHANICS,2023,974:32.Rp_Au:Dong, Ming, Zhao, Lei
APA 纪晓阳,董明,&Zhao, Lei.(2023).Impact of compliant coating on Mack-mode evolution in hypersonic boundary layers.JOURNAL OF FLUID MECHANICS,974,32.
MLA 纪晓阳,et al."Impact of compliant coating on Mack-mode evolution in hypersonic boundary layers".JOURNAL OF FLUID MECHANICS 974(2023):32.
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