Finite element simulation of a space shuttle solid rocket booster aft skirt splashdown using an arbitrary Lagrangian-Eulerian approach

Finite element simulation of a space shuttle solid rocket booster aft skirt splashdown using an arbitrary Lagrangian-Eulerian approach /

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Bibliographic Details
Main Author: Melis, Matthew E.
Corporate Author: NASA Glenn Research Center
Format: Government Document Book
Language:English
Published: [Cleveland, Ohio] : [NASA Glenn Research Center], [2003]
[Cleveland, Ohio] : [2003]
Series:NASA technical memorandum 212093.
Subjects:
Euler-Lagrange equation.
Finite element method.
Skirts.
Space Shuttle Boosters.
Water landing.
Description
Item Description:Shipping list no.: 2003-0488-M.
"January 2003."
Physical Description:1 volume.
Also available via Internet from the NTRS web site. Address as of 1/5/05: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/20030016601%5F2003020325.pdf; current access is available via PURL.

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