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An experimental investigation of hypersonic flow over blunt nosed cones at a Mach number of 5.8 /

Thesis (Aeronautical Engineer). / Includes bibliographical references.

Identiferoai:union.ndltd.org:OCLC/oai:xtcat.oclc.org:OCLCNo/437065451
Date January 1956
CreatorsO'Bryant, William T. Lees, Lester,
PublisherPasadena, Calif. : California Institute of Technology,
Source SetsOCLC
LanguageEnglish
Detected LanguageEnglish
TypeElectronic dissertations.
Source<a href="http://resolver.caltech.edu/CaltechETD:etd-06182004-111807" TARGET="_blank">An experimental investigation of hypersonic flow over blunt nosed cones at a Mach number of 5.8 [electronic thesis]</a>

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