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International Journal of Crashworthiness Volume 20, 2015 - Issue 5
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Original Articles

Parametrised fuselage modelling to evaluate aircraft crash behaviour in early design stages

Dominik B. SchwinnDepartment of Structural Integrity, Institute of Structures and Design (BT), German Aerospace Center (DLR), Stuttgart, GermanyCorrespondence[email protected]
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Pages 413-430 | Received 01 Oct 2014, Accepted 19 Feb 2015, Published online: 26 Mar 2015

Citations (4)

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Read on this site (1)

M. H. Siemann, D. B. Schwinn, J. Scherer & D. Kohlgrüber. (2018) Advances in numerical ditching simulation of flexible aircraft models. International Journal of Crashworthiness 23:2, pages 236-251.
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Articles from other publishers (3)

Zibo Jin, Daochun Li & Jinwu Xiang. (2020) Crash simulation of fuselage section in the rebound process and the secondary-impact process. Aircraft Engineering and Aerospace Technology 92:8, pages 1245-1256.
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D. B. Schwinn, D. Kohlgr?ber, J. Scherer & M. H. Siemann. (2016) A parametric aircraft fuselage model for preliminary sizing and crashworthiness applications. CEAS Aeronautical Journal 7:3, pages 357-372.
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Dominik B. Schwinn. (2015) Applied parametrized and automated airframe modeling methods in the preliminary design phase. International Journal of Modeling, Simulation, and Scientific Computing 06:04, pages 1550037.
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