Finite element simulation of a space shuttle solid rocket booster aft skirt splashdown using an arbitrary Lagrangian-Eulerian approach
By: Matthew E. Melis.
Contributors: NASA Glenn Research Center.
Series: NASA/TM -- 2003-212093.; NASA technical memorandum -- 212093.
Publisher: NASA Glenn Research Center
Published: 2003
Place of publication: [Cleveland, Ohio
Language: eng
Format: Microform
Subjects: Euler-Lagrange equation.; Finite element method.; Skirts.; Space shuttle boosters.; Water landing.
Notes: Shipping list no.: 2003-0488-M.

"January 2003."

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.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 2003]