Please use this identifier to cite or link to this item: http://hdl.handle.net/10397/93034
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dc.contributorDepartment of Mechanical Engineeringen_US
dc.creatorTian, Xen_US
dc.creatorZhao, Ren_US
dc.creatorLong, Ten_US
dc.creatorWen, CYen_US
dc.date.accessioned2022-05-30T07:40:12Z-
dc.date.available2022-05-30T07:40:12Z-
dc.identifier.issn0001-1452en_US
dc.identifier.urihttp://hdl.handle.net/10397/93034-
dc.language.isoenen_US
dc.publisherAmerican Institute of Aeronautics and Astronauticsen_US
dc.rightsCopyright © 2019 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.en_US
dc.rightsThis is the peer reviewed version of the following article: Tian, X., Zhao, R., Long, T., & Wen, C. Y. (2019). Reverse design of ultrasonic absorptive coating for the stabilization of Mack modes. AIAA Journal, 57(6), 2264-2269, which has been published in final form at https://doi.org/10.2514/1.J058105.en_US
dc.subjectCompressible boundary layeren_US
dc.subjectFreestream mach numberen_US
dc.subjectThermal protection systemen_US
dc.subjectFlow conditionsen_US
dc.subjectTemperature ratioen_US
dc.subjectFlow velocityen_US
dc.subjectAngle of attacken_US
dc.subjectNavier stokes equationsen_US
dc.subjectHypersonic transportsen_US
dc.subjectCollocation methoden_US
dc.titleReverse design of ultrasonic absorptive coating for the stabilization of mack modesen_US
dc.typeJournal/Magazine Articleen_US
dc.identifier.spage2264en_US
dc.identifier.epage2269en_US
dc.identifier.volume57en_US
dc.identifier.issue6en_US
dc.identifier.doi10.2514/1.J058105en_US
dcterms.abstractThe effects of ultrasonic absorptive coating (UAC) admittance on the first and second modes in a high-speed boundary layer are analyzed using linear stability theory. It is shown that the growth rate of the first mode is increased as UAC admittance phase θ varies from 0.5π to π, whereas the second mode is amplified when θ tends to 0.5π and damped if θ ≥ 0.75π. The frequency range of the first mode is broadened when θ is in the vicinity of π, and the second mode shifts to low frequencies when θ < π. Moreover, the stabilization or destabilization effects on Mack modes, frequency band broadening, and frequency shifting are promoted by large UAC admittance magnitudes. Based on the requirements of the admittance phase and magnitude for the stabilization of Mack modes, a design strategy for UAC is proposed to stabilize the second mode in a wide frequency range with the first mode little amplified.en_US
dcterms.accessRightsopen accessen_US
dcterms.bibliographicCitationAIAA journal, June 2019, v. 57, no. 6, p. 2264-2269en_US
dcterms.isPartOfAIAA journalen_US
dcterms.issued2019-06-
dc.identifier.scopus2-s2.0-85067035588-
dc.identifier.eissn1533-385Xen_US
dc.description.validate202205 bchyen_US
dc.description.oaAccepted Manuscripten_US
dc.identifier.FolderNumberME-0537-
dc.description.fundingSourceRGCen_US
dc.description.fundingSourceOthersen_US
dc.description.fundingTextNatural Science Foundation of Chinaen_US
dc.description.pubStatusPublisheden_US
dc.identifier.OPUS20515874-
dc.description.oaCategoryGreen (AAM)en_US
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