A Thermodynamically Consistent Damage Model for Advanced Composites

By: Administration (Nasa), National Aeronaut

Technical Report Maimi, Pere and Camanho, Pedro P. and Mayugo, Joan-Andreu and Davila, Carlos G. Langley Research Center NASA/TM-2006-214282, L-19239 COMPOSITE MATERIALS; DAMAGE; CONTINUUM MODELING; FIBER COMPOSITES; CRACK CLOSURE; DEGRADATION; LOADS (FORCES); PREDICTIONS; NUMERICAL ANALYSIS; MATHEMATICAL MODELS

• Format: Paperback
• Language: English
• ISBN: B08F6CGBT3
• ISBN13: 9798673043547
• Release Date: January 1
• Publisher: Independently Published
• Length: 48 Pages
• Weight: 0.30 lbs.
• Dimensions: 0.1" x 8.5" x 11.0"