Author:
Shoji Hirokazu,Minegishi Masakatsu,Aoki Takahira
Publisher
American Institute of Aeronautics and Astronautics
Reference6 articles.
1. 1Kumakura, I., Minegishi, M., Iwasaki, K., Shoji, H., Yoshimoto, N., Sashikuma, H., Isoe, A., Yamaoka, T., Katayama, N., Hayashi, T., and Akaso, T. "Vertical Drop Test of a Transport Fuselage Section," SAE World Aviation Congress 2002, Paper No.2002-01-2997,2002.
2. 3Kim, H.S., and Wierzbicki, T. "Closed-form solution for crushing response of three-dimensional thin-walled "S" frames with rectangularcross-sections,"InternationalJournal of ImpactEngineering, Vol.30,2004, pp.87-112.
3. Energy absorption of metallic cylindrical shells with induced non-axisymmetric folding patterns
4. The Ultimate Strength of Aluminum-Alloy Formed Structural Shapes in Compression
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6 articles.
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