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Shock interaction due to blunt leading edges of two-dimensional hypersonic inlets.

No description available.
Identiferoai:union.ndltd.org:mcgill.ca/oai:escholarship.mcgill.ca:sb397963c
Date January 1969
CreatorsO'Connell, Kevin John.
PublisherMcGill University
Source SetsMcGill University
Languagehttp://id.loc.gov/vocabulary/iso639-2/eng
Detected LanguageEnglish
TypeThesis
RightsAll items in eScholarship@McGill are protected by copyright with all rights reserved unless otherwise indicated.
RelationProquest: AAIMK06029, Pid: 49033

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