Underwater Shock Analysis of a Missile Launch Tube.
Abstract
This report documents the results of a non-linear, elastic-plastic, structural response analysis of a missile launch tube to underwater shock. The analysis was performed with the structural response code USA-STAGS. This code employs the finite element method for the structure and the Doubly Asymptotic Approximation (DAA) for the fluid-structure interaction. This analysis was performed in support of a General Dynamics/Electric Boat Division design development for an upcoming shock test to be conducted by the Navy. This report is intended to document results to date in this support effort.
Document Details
- Document Type
- Technical Report
- Publication Date
- May 20, 1982
- Accession Number
- ADA122288
Entities
People
- Kenneth C. Kiddy
Organizations
- Naval Ordnance Laboratory