Vertical Drop Test of Composite Fuselage Section of a Regional Aircraft
Author:
Affiliation:
1. Leonardo Company Aircraft Division, Pomigliano d’Arco 80038, Italy
Funder
Italian Ministry of Research
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference15 articles.
1. Optimization of Helicopter Subfloor Components Under Crashworthiness Requirements Using Neural Networks
2. Full-scale crash test and simulation of a composite helicopter
3. Research on Effects of Oblique Struts on Crashworthiness of Composite Fuselage Sections
4. Development of a Scale Model Composite Fuselage Concept for Improved Crashworthiness
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