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Temperature distribution in the boundary layer of an airplane wing with a line source of heat at the stagnation edge. Part 1. Symmetric wing in symmetric flow

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dc.contributor.authorYih, Chia-shun, 1918-1997, author
dc.contributor.authorCermak, J. E. (Jack E.), author
dc.contributor.authorShen, Richard Tsu-hsun, author
dc.contributor.authorCivil Engineering Department, Colorado Agricultural and Mechanical College, publisher
dc.date.accessioned2017-09-29T14:31:22Z
dc.date.available2017-09-29T14:31:22Z
dc.date.issued1952-10
dc.descriptionCER53CSY5.
dc.descriptionOctober, 1952.
dc.descriptionIncludes bibliographical references.
dc.format.mediumreports
dc.identifier.urihttps://hdl.handle.net/10217/184170
dc.languageEnglish
dc.language.isoeng
dc.publisherColorado State University. Libraries
dc.relationCatalog record number (MMS ID): 991012973789703361
dc.relationTA7.C6 CER 53-5
dc.relation.ispartofCivil Engineering Reports
dc.relation.ispartofCER, 53-5
dc.rightsCopyright and other restrictions may apply. User is responsible for compliance with all applicable laws. For information about copyright law, please see https://libguides.colostate.edu/copyright.
dc.subjectBoundary layer
dc.subjectAirplanes -- Wings
dc.subjectFluid dynamics
dc.titleTemperature distribution in the boundary layer of an airplane wing with a line source of heat at the stagnation edge. Part 1. Symmetric wing in symmetric flow
dc.title.alternativeSymmetric wing in symmetric flow
dc.typeText
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