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Impact Simulation of Simplified Structural Models of Aircraft Fuselage National Aerospace Laboratory, Japan
- Format:
- Book
- Conference/Event
- Author/Creator:
- Kumakura, Ikuo, author.
- Conference Name:
- World Aviation Congress & Exposition (2000-10-10 : San Diego, California, United States)
- Language:
- English
- Physical Description:
- 1 online resource cm
- Place of Publication:
- Warrendale, PA SAE International 2000
- Summary:
- For ensuring occupant's survivability in case of aircraft crash accident, it is necessary to alleviate the impact load to an allowable level of the human body. This research aims to develop the analytical models for simulation of impact characteristics of aircraft fuselage structure. The numerical analysis on the sub-floor structures was executed by using nonlinear dynamic analysis code LS-DYNA3D, and the results of analytical models are evaluated using the results of crash tests of structural models
- Notes:
- Vendor supplied data
- Publisher Number:
- 2000-01-5586
- Access Restriction:
- Restricted for use by site license
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