A Numerical Simulation of Axisymmetric Solid Rocket Motor Ignition Transient with Radiation Effect

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dc.contributor.authorCho, IH-
dc.contributor.authorBaek, Seung-Wook-
dc.contributor.authorChang, ST-
dc.date.accessioned2013-03-15T13:14:29Z-
dc.date.available2013-03-15T13:14:29Z-
dc.date.created2012-02-06-
dc.date.issued1996-07-
dc.identifier.citationThe 32nd AIAA/ASME/SAE/ ASEE Joint Propulsion Conference, v., no., pp. --
dc.identifier.urihttp://hdl.handle.net/10203/119761-
dc.languageENG-
dc.titleA Numerical Simulation of Axisymmetric Solid Rocket Motor Ignition Transient with Radiation Effect-
dc.typeConference-
dc.type.rimsCONF-
dc.citation.publicationnameThe 32nd AIAA/ASME/SAE/ ASEE Joint Propulsion Conference-
dc.identifier.conferencecountryUnited States-
dc.identifier.conferencecountryUnited States-
dc.contributor.localauthorBaek, Seung-Wook-
dc.contributor.nonIdAuthorCho, IH-
dc.contributor.nonIdAuthorChang, ST-
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AE-Conference Papers(학술회의논문)
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