A Procedure for Modeling Structural Component/Attachment Failure Using Transient Finite Element Analysis

By: Administration (Nasa), National Aeronaut

Technical Report Lovejoy, Andrew E. and Jegley, Dawn C. (Technical Monitor) Langley Research Center NASA/CR-2007-214540 NNL04AA10B; WBS 561581.02.08.07 TRANSIENT RESPONSE; STATIC LOADS; FAILURE ANALYSIS; STRUCTURAL FAILURE; TIME DEPENDENCE; STABILIZERS (FLUID DYNAMICS)

• Format: Paperback
• Language: English
• ISBN: B08F6X4PLL
• ISBN13: 9798672848013
• Release Date: January 1
• Publisher: Independently Published
• Length: 42 Pages
• Weight: 0.27 lbs.
• Dimensions: 0.1" x 8.5" x 11.0"