An alternative numerical approach for full scale characterisation for riveted joint design

Aerospace Science and Technology

Volumn 6, Issue 5, 2002, Pages 343-354

  Langrand, B ^a   Patronelli, L ^a   Deletombe, E ^a   Markiewicz, E ^b   Drazetic P ^b  

^a ONERA   (France)

^b UNIVERSITÉ DE VALENCIENNES   (France)

Author keywords

Airframe crashworthiness; Dynamic strength; Embrittlement; Equivalent modelling; Failure criterion; FE modelling; Riveted joints

Indexed keywords

AIRFRAMES; COMPUTER SIMULATION; CRACK PROPAGATION; CRASHWORTHINESS; EMBRITTLEMENT; JOINTS (STRUCTURAL COMPONENTS); RIVETING; STRENGTH OF MATERIALS;

DYNAMIC STRENGTH; RIVETED JOINTS;

AEROSPACE ENGINEERING;

EID: 0036389827     PISSN: 12709638     EISSN: None     Source Type: Journal    
DOI: 10.1016/S1270-9638(02)01174-4     Document Type: Article

References (22)

1. B. Langrand, L. Patronelli, E. Deletombe et al., Full scale experimental characterisation for riveted joint design, Aerospace Science and Technology.
2. B. Langrand, Experimental characterisation of aluminium alloys 2042-T351 and 7050, Technical Report n°97/54, DMSE/RCS, ONERA, October 1997.
3. L. Patronelli, B. Langrand, E. Deletombe, et al., New experimental procedure for analysis of rivet material mechanical properties, CEAS Forum, Crash Questions, Naples, Italy, 2000.
4. A.L. Gurson, Continuum theory of ductile rupture by void nucleation and growth. Part 1: yield criteria and flow rules for porous ductile media, J. Engrg. Mater. Tech. ASME 99 (1977) 2-15.
5. V. Tvergaard, A. Needleman, Analysis of cup-one fracture in a round tensile bar, Acta Metalurgica 32 (1987) 157-169.
6. Pam-Crash User's Manual, 20 rue Saarinen, Silic 303, 94588 RungisCedex, France.
7. F. Lauro, B. Bennani, P. Drazétic, J. Oudin, X. Ni, Ductile damage and fracture finite element modelling of elasto-viscoplastic voided materials. Computational Materials Science 7 (1997) 295-307.
8. B. Langrand, E. Deletombe, E. Markiewicz, P. Drazétic, Numerical approach for assessment of dynamic strength for riveted joints, Aerospace Science and Technology 3 (1999) 431-446.
9. US military standard, Rivets, buck type, preparation for and installation of, Ref. MIL-R-47196A-NOTICE 1, June 1986.
10. US military standard, Military standard, preparation for and installation of, Ref. MIL-STD-403C-14, June 1992.
11. E. Deletombe, P. Geoffroy, IMT Crashworthiness for commercial aircraft - Static test I - Numerical analysis. Technical Report n°93/63, 1993.
12. E. Deletombe, IMT Crashworthiness for commercial aircraft - Finite element modelling of riveted joints and plastic hinges, Technical Report n°96/25, 1996.
13. L. Arcan, M. Arcan, I.M. Daniel, SEM fractography of pure and mixed mode interlaminar fracture in Graphite/Epoxy composites, ASTM Special Technical Publication, No. 948, 1987, 41-47.
14. M. Muller-Bechtel, Schweibpunktversagen in der FE crash simulation, Diplomarrbeit, 1994, in german.
15. K. Schweizerhok, T. Engleder, Crashworthiness programme for commercial aircraft - Subtask 2.2 Modelling in Crashworthiness analysis, CAD-FEM Technical Report n°AERO-95-3, December 1995.
16. G. Winkelmuller, Crashworthiness for commercial aircraft - 24 month progress report, Mecalog Project E422/92, January 1995.
17. P. Ducrocq, New approaches to improve the representativeness of finite element models in Crashworthiness events, Ph.D. Thesis, University of Valenciennes, 1997.
18. A. Juanicotena, B. Malherbe, On the modelling of riveted joints by beam type spring element in Radioss Crash code - Application to the crash of an aeronautical substructure, IRUC/IRUM Conference, Sophia-Antipolis, France, 1999.
19. B. Malherbe, B. Langrand, J.-L. Charles, J.-F. Sobry, Improvement of crash models of large aeronautical structures, 22nd ICAS Congress, Harrogate, Great Britain, 2000.
20. R. Hashemi, Crashworthiness for commercial aircraft - Subtask 2.4 Sub component quasi-static tests on an Airbus A320 rear fuselage, Cranfield Impact Centre, AER2-CT92-0030, March 1994.
21. R. Hashemi, Crashworthiness for commercial aircraft - Subtask 2.4 Sub component dynamic tests on an Airbus A320 rear fuselage, Cranfield Impact Centre, AER2-CT92-0030, December 1994.
22. L. Patronelli, B. Langrand, E. Deletombe, et al., Structural embrittlement due to riveted joints - Evolution to a macroscopic model for crash analysis, The Fifth International Conference on Computational Structures Technology, Leuven, Belgium, 2000.