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Coupling of Fluid Thermal Simulation for Nonablating Hypersonic Reentry Vehicles Using Commercial Codes FLUENT and LS-DYNA

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Identiferoai:union.ndltd.org:OhioLink/oai:etd.ohiolink.edu:ucin1218801526
Date22 September 2008
CreatorsSockalingam, Subramani
PublisherUniversity of Cincinnati / OhioLINK
Source SetsOhiolink ETDs
LanguageEnglish
Detected LanguageEnglish
Typetext
Sourcehttp://rave.ohiolink.edu/etdc/view?acc_num=ucin1218801526
Rightsunrestricted, This thesis or dissertation is protected by copyright: all rights reserved. It may not be copied or redistributed beyond the terms of applicable copyright laws.

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