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College of Engineering(공과대학)School of Mechanical and Aerospace Engineering(기계항공공학부)Dept. of Aerospace Engineering(항공우주공학과)AE-Conference Papers(학술회의논문)

Numerical Analysis of Ignition Transient in an Axisymmetric Solid Rocket Motor Equipped with Rear Ignition System

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dc.contributor.authorBaek, Seung-Wook-
dc.contributor.authorCho, IH-
dc.date.accessioned2013-03-15T13:15:04Z-
dc.date.available2013-03-15T13:15:04Z-
dc.date.created2012-02-06-
dc.date.issued1997-07-
dc.identifier.citation33rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, v., no., pp. --
dc.identifier.urihttp://hdl.handle.net/10203/119764-
dc.languageENG-
dc.titleNumerical Analysis of Ignition Transient in an Axisymmetric Solid Rocket Motor Equipped with Rear Ignition System-
dc.typeConference-
dc.type.rimsCONF-
dc.citation.publicationname33rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit-
dc.identifier.conferencecountryUnited States-
dc.identifier.conferencecountryUnited States-
dc.contributor.localauthorBaek, Seung-Wook-
dc.contributor.nonIdAuthorCho, IH-
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AE-Conference Papers(학술회의논문)
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