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dc.contributor.authorEarl A. Thornton
dc.date.accessioned2017-05-08T23:52:15Z
dc.date.available2017-05-08T23:52:15Z
dc.date.copyrightSeptember, 1997
dc.date.issued1997
dc.identifier.issn0003-6900
dc.identifier.otherAMREAD-25734#477_1.pdf
dc.identifier.urihttp://yetl.yabesh.ir/yetl/handle/yetl/118032
dc.description.abstractThis review article describes aerospace thermal-structural testing technology. It begins with discussions of aerodynamic heating and space radiation heating. The review continues with a general discussion of thermal-structural test technology including heating and cooling, instrumentation, and thermal-structural boundary conditions. Then illustrative thermal structural tests are presented for high speed flight in the atmosphere and flight in space. Experiments conducted in the laboratory as well as flight tests are described. Several experiments are reviewed to demonstrate the diversity of thermal-structural phenomena. This article includes 120 references.
dc.publisherThe American Society of Mechanical Engineers (ASME)
dc.titleAerospace Thermal-Structural Testing Technology
dc.typeJournal Paper
dc.journal.volume50
dc.journal.issue9
dc.journal.titleApplied Mechanics Reviews
dc.identifier.doi10.1115/1.3101738
dc.journal.fristpage477
dc.journal.lastpage498
dc.identifier.eissn0003-6900
dc.keywordsAerospace industry
dc.keywordsTesting
dc.keywordsFlight
dc.keywordsHeating
dc.keywordsExtraterrestrial radiation
dc.keywordsBoundary-value problems
dc.keywordsHeating and cooling AND Instrumentation
dc.treeApplied Mechanics Reviews:;1997:;volume( 050 ):;issue: 009
dc.contenttypeFulltext


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