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Impact pressure and total temperature interpretation at hypersonic Mach number /

Thesis (Aeronautical Engineer). / Includes bibliographical references.

Identiferoai:union.ndltd.org:OCLC/oai:xtcat.oclc.org:OCLCNo/437061446
Date January 1954
CreatorsGraves, Jack C. Nagamatsu, Henry T.,
PublisherPasadena, Calif. : California Institute of Technology,
Source SetsOCLC
LanguageEnglish
Detected LanguageEnglish
TypeElectronic dissertations.
Source<a href="http://resolver.caltech.edu/CaltechETD:etd-12182003-100211" TARGET="_blank">Impact pressure and total temperature interpretation at hypersonic Mach number [electronic thesis]</a>

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