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Measurement of heat transfer on a flat plate-step model at Mach 14: (Task 3.4--shock tunnel experiments--REST Project)

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dc.contributor.authorSandborn, Virgil A., author
dc.contributor.authorHeron K., author
dc.contributor.authorResearch and Advanced Development Divison, AVCO Corp., publisher
dc.date.accessioned2019-09-17T18:54:49Z
dc.date.available2019-09-17T18:54:49Z
dc.date.issued1963-06
dc.descriptionCER63VAS80.
dc.description26 June 1963.
dc.descriptionPrepared for Air Force Ballistic Systems Division, Air Force Systems Command, United States Air Force, Norton Air Force Base, California.
dc.descriptionIncludes bibliographical references.
dc.description.sponsorshipUnder Contract no AF04(694)-239.
dc.format.mediumtechnical reports
dc.identifier.urihttps://hdl.handle.net/10217/198008
dc.languageEnglish
dc.language.isoeng
dc.publisherColorado State University. Libraries
dc.relationCatalog record number (MMS ID): 991013215549703361
dc.relation.ispartofCivil Engineering Reports
dc.relation.ispartofTechnical memorandum, RAD-TM-63-40
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.subjectFluid mechanics
dc.subjectHeat -- Transmission
dc.subjectHypersonic wind tunnels
dc.titleMeasurement of heat transfer on a flat plate-step model at Mach 14: (Task 3.4--shock tunnel experiments--REST Project)
dc.typeText
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