Modelling of impact forces and pressures in Lagrangian bird strike analyses

Author:

Airoldi A.,Cacchione B.

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,Ocean Engineering,Safety, Risk, Reliability and Quality,Aerospace Engineering,Automotive Engineering,Civil and Structural Engineering

Reference16 articles.

1. Brockman RA, Held TW. Explicit finite element method for transparency impact analysis. University of Dayton Research Institute Report WL-TR-91-3006, 1991

2. McCarty RE. Finite element analysis of F-16 aircraft canopy dynamic response to bird impact loading. AIAA Paper AIAA 80-0804. 21st structures, structural dynamics, and materials conference. Seattle, WA, USA: 1980.

3. Modelling soft body impact on composite structures;Johnson;Compos Struct,2003

4. Airoldi A, Tagliapietra D. Bird impact simulation against a hybrid composite and metallic vertical stabilizer. AIAA Paper AIAA 2001-1390, 42nd AIAA/ASME/ASCE/AHS/ASC structures, structural dynamics, and materials conference and exhibit. Seattle. WA, USA: 2001.

5. Gong YN, Qian C. New model of bird impact response analysis and its engineering solution. In: Proceedings of the 18th ICAS congress.vol 2. . 1992. p. 1476–81.

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