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

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]
Series:	NASA technical memorandum ; 212093.
Subjects:	Euler-lagrange equation. finite element method. Skirts. SPACE SHUTTLE BOOSTERS. Water landing.
Online Access:	https://purl.fdlp.gov/GPO/LPS56853