Crashworthiness Optimization of Aircraft Hybrid Energy Absorbers Enclosing Honeycomb and Foam Structures
Author:
Affiliation:
1. Universidade da Coruña, 15071 A Coruña, Spain
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J055245
Reference32 articles.
1. De FlorioF., Airworthiness: An Introduction to Aircraft Certification, Butterworth-Heinemann, Oxford, 2006, pp. 33–43.
2. Multi-Terrain Impact Tests and Simulations of an Energy Absorbing Fuselage Section
3. Improvement of crashworthiness behaviour for simplified structural models of aircraft fuselage
4. Finite element methodologies development to simulate the behaviour of composite fuselage structure and correlation with drop test
5. Optimal design of composite fuselage frames for crashworthiness
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