Finite element simulation of a space shuttle solid rocket booster aft skirt splashdown using an arbitrary Lagrangian-Eulerian approach
An edition of Finite element simulation of a space shuttle solid rocket booster aft skirt splashdown using an arbitrary Lagrangian-Eulerian approach (2003)
By Matthew E. Melis
Publish Date
2003
Publisher
NASA Glenn Research Center
Language
eng
Pages
-
Description: