Explicit Finite-Element Analysis of 2024-T3/T351 Aluminum Material under Impact Loading for Airplane Engine Containment and Fragment Shielding
symposium, Ballistic impact and crashworthiness analysis of aerospace structures (Symposium) ; 2008 ; Long Beach, CA
2009-01-01
9 pages
Conference paper
English
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Notch Size Effects in 2024-T351 Aluminum Alloy Under Fatigue Spectrum Loading
British Library Online Contents | 1998
|Notch Size Effects in 2024-T351 Aluminum Alloy Under Fatigue Spectrum Loading
Online Contents | 1998
|