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

Saved in:

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.

University of Minnesota

Holdings details from University of Minnesota
Call Number:	Mfiche NAS 1.15:212093