Recent developments in modelling and experimentation fields with respect to crashworthiness and impact on aerospace structures

ECCOMAS 2004 - European Congress on Computational Methods in Applied Sciences and Engineering

Volumn , Issue , 2004, Pages

  Deletombe, E ^a   Delsart, D ^a   Fabis, J ^a   Langrand, B ^a   Ortiz, R ^a  

^a ONERA   (France)

Author keywords

Crashworthiness; Dynamic tests; Finite element models; Non linear behaviours; Vulnerability

Indexed keywords

AEROSPACE STRUCTURE; DYNAMIC TESTS; EXPERIMENTAL DEVELOPMENT; MATERIAL CHARACTERISTICS; NONLINEAR BEHAVIOURS; STRENGTH CHARACTERISTICS; STRUCTURAL PROBLEMS; VULNERABILITY;

AIRCRAFT ACCIDENTS; COMPUTATIONAL METHODS; FINITE ELEMENT METHOD; SPACE RESEARCH; STRENGTH OF MATERIALS; STRUCTURAL DYNAMICS;

CRASHWORTHINESS;

EID: 84893445279     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (14)

1. E. Deletombe. Fluid-Structure simulation of hydraulic ram pressure in fuel tanks. Engineering Computational Technology 98, Edinburgh, 1998.
2. nd ONERA-DLR Aerospace Symposium, Berlin (G), 2000.
3. B. Langrand, E. Markiewicz, P. Drazétic, P. Geoffroy, J.-L. Petitniot and J. Fabis. Constitutive models characterisation for XC48 steel in compression by a parametric identification technique. International Journal of Materials and Product Technology, Vol. 12, No4-6, pp. 428-446, 1997.
4. G. Haugou, J. Fabis, B. Langrand, E. Deletombe and E. Markiewicz. Iterative experimental vs numerical procedure for improvement of dynamic experimental facilities. SUSI 2002, Structures under Shock and Impact. Montréal, 27-29 mai 2002, TP 2002-149, 2002.
5. E. Deletombe, D. Delsart, D. Kohlgrüber and A.F. Johnson. Improvement of numerical methods for crash analysis in future composite aircraft design. Aerospace Science and Technology, Vol. 4, pp. 189-199, 2000, TP 2000-235, 2000.
6. nd ICAS Congress, Harrogate (U.K.), 2000.
7. B. Langrand, E. Deletombe, E. Markiewicz and P. Drazetic. Riveted joint modelling for numerical analysis of airframe crashworthiness. Finite Element in Analysis and Design, 38, 21-44, 2001.
8. B. Langrand, L. Patronelli, E. Deletombe, E. Markiewicz and P. Drazetic. An alternative numerical approach for full scale characterisation for riveted joint design. Aerospace Science and Technology, 6(5), 343-354, 2002.
9. B. Langrand, E. Deletombe, E. Markiewicz and P. Drazetic. Characterisation of dynamic failure for riveted joint assemblies. Shocks and Vibration, 7, 121-138, 2000.
10. B. Langrand, L. Patronelli, E. Deletombe, E. Markiewicz and P. Drazetic. Full scale experimental characterisation for riveted joint design. Aerospace Science and Technology, 6(5), 333-342, 2002.
11. L. Patronelli, B. Langrand, E. Deletombe, E. Markiewicz and P. Drazetic. Structural embrittlement due to riveted joints evolution to a macroscopic model for crash analysis. Computational Techniques for Materials, Composites and Composite Structures. Edited by B.H.V. Topping, 103-109, 2000.
12. L. Patronelli, A.S. Bayart, B. Langrand, E. Deletombe, E. Markiewicz and P. Drazetic. Structural embrittlement due to the punchings of riveted joints. Mécanique & Industries, 4(1), 29-39, 2002.
13. G. Portemont, R. Ortiz and P. Drazetic. Assesment of basic experimental impact simulations for coupled fluid/structure interactions modelling. International Crash and Design Symposium, Lille, 2003.
14. B. Langrand, A-S. Bayart, Y. Chauveau and E. Deletombe. Assessment of multi-physics FE methods for bird strike modelling - Application to a metallic riveted airframe. Int. J. of Crashworthiness, 7(4) 415-427, 2002.