NUMERICAL SIMULATION OF A COMPOSITE HELICOPTER SUB-FLOOR STRUCTURE SUBJECTED TO WATER IMPACT

VFS-F60-000118

6/7/2004

Authors
Abstract
Content

This paper describes recent research activities on the design, numerical simulation and testing of a composite helicopter sub-floor structure with a novel approach to avoid skin breakage in the case of a crash on water. After the analysis of the structural behavior of current sub-floor designs in the case of water crash events IAI and ECD worked on a new design which was supported by numerical simulation work performed by DLR using the explicit FE-codes PAM-CRASH. Finally a demonstrator sub-floor box was built to prove the concept in a component test that was performed at CIRA. In this paper the entire study is presented with a focus on the numerical crash simulations and the comparison with the corresponding test results from a purely vertical drop test on water. Finally, the validated simulation approach is used in a sensitivity study to investigate the behavior of the new sub-floor design in load cases with initial pitch and roll angles that could not be tested.

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DOI
https://doi.org/10.4050/VFS-F60-000118
Citation
Kohlgrüber, D., Vigliotti, A., Weissberg, V., and Bartosch, H., "NUMERICAL SIMULATION OF A COMPOSITE HELICOPTER SUB-FLOOR STRUCTURE SUBJECTED TO WATER IMPACT," Forum 60 - Baltimore, MD 2004, Baltimore, Maryland, June 7, 2004, https://doi.org/10.4050/VFS-F60-000118.
Additional Details
Publisher
Published
6/7/2004
Product Code
VFS-F60-000118
Content Type
Technical Paper
Language
English