Conceptual studies of a composite-aluminum hybrid wing box demonstrator

Aerospace Science and Technology

Volumn 32, Issue 1, 2014, Pages 42-50

  Kapidžić, Zlatan ^a,b   Nilsson, Larsgunnar ^b   Ansell, Hans ^a  

^a SAAB AB   (Sweden)

^b LINKÖPING UNIVERSITY   (Sweden)

Author keywords

Composite aluminum; Conceptual study; Hybrid structure; Thermal load; Wing structure

Indexed keywords

AIRCRAFT INDUSTRIES; COMPOSITE-ALUMINUM; CONCEPTUAL STUDY; HYBRID STRUCTURE; STRUCTURAL BEHAVIORS; STRUCTURAL FATIGUE; THERMAL BEHAVIORS; WING STRUCTURES;

BOLTED JOINTS; BUCKLING; THERMAL LOAD;

ALUMINUM;

EID: 84892551354     PISSN: 12709638     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.ast.2013.11.002     Document Type: Article

References (25)

1. V. Caccese, J.P. Kabche, and K.A. Berube Analysis of a hybrid composite/metal bolted connection subjected to flexural loading Compos. Struct. 81 2007 450 462
2. V. Caccese, J.P. Kabche, K.A. Berube, and M.J. Boone Structural response of a hybrid composite/aluminum strut assembly Compos. Struct. 80 2007 159 171
3. C.S. Collier Stiffness, thermal expansion, and thermal bending formulation of stiffened, fiber-reinforced composite panels La Jolla, CA 34th SDM Conference 1993
4. J. Ekh, and J. Schön Effect of secondary bending on strength prediction of composite, single shear lap joints Compos. Sci. Technol. 65 2005 953 965
5. ESDU 89046, Fatigue of aluminum alloy joints with various fastener systems, Low load transfer, 1989.
6. FALSTAFF, Description of a fighter aircraft loading standard for fatigue Joint publication of Flugzeugwerke Emmen (F+W), Switzerland, Laboratorium für Betriebsfestigkeit (LBF), Darmstadt, Germany, National Aerospace Laboratory (NLR), Amsterdam, Netherlands, and Industrie-Anlagen- Betriebsgesellschaft mbH (IABG), Ottobrunn, Germany 1976
7. Federal Aviation Administration, Advisory Circular No:20-107A, 4/25/84.
8. T.J.R. Huges The Finite Element Method: Linear Static and Dynamic Finite Element Analysis 2000 Dover Publications New York
9. D. Hull, and T.W. Clyne An Introduction to Composite Materials second ed. 1996 Cambridge University Press Cambridge
10. T. Ireman, T. Nyman, and K. Hellbom On design methods for bolted joints in composite aircraft structures Compos. Struct. 25 1993 567 578
11. J.P. Kabche, V. Caccese, K.A. Berube, L. Thompson, and J. Walls Structural response of a hybrid composite-to-metal bolted connection under uniform pressure loading Compos. Struct. 78 2007 207 221
12. H.S. Kim, and D.G. Lee Optimal design of the press fit joint for a hybrid aluminum/composite drive shaft Compos. Struct. 70 2005 33 47
13. D.G. Lee, H.S. Kim, J.W. Kim, and J.K. Kim Design and manufacture of an automotive hybrid aluminum/composite drive shaft Compos. Struct. 63 2004 87 99
14. Military Handbook, Polymer Matrix Composites MIL-HDBK-17-3F 2000 U.S. Department of Defense
15. M.C.Y. Niu Airframe Structural Design second ed. 1999 Hong Kong Conmilit Press Hong Kong
16. J.N. Reddy Mechanics of Laminated Composite Plates and Shells: Theory and Analysis second ed. 2004 CRC Press Boca Raton
17. J. Rouchon Certification of large airplane composite structures - Recent progress and new trends in compliance philosophy Stockholm Proc. 17th ICAS Congress 1990 paper ICAS-90-1.8.1
18. J. Rouchon, Fatigue and damage tolerance evaluation of structures: The composite material response, in: 22th Plantema Memorial Lecture, 25th ICAF Symposium, Rotterdam, 2009.
19. Simulia Abaqus Analysis User's Manual www.simulia.com 2011
20. I.C. Skrna-Jakl, M.A. Stiftinger, and F.G. Rammerstorfer Numerical investigations of an imperfect stringer-stiffened composite wing torsion box - an analysis concept Composites, Part B 27B 1996 59 69
21. M.B. Snell, and P. Bartholomew The engineering optimisation of hybrid composite/metallic wing boxes for buckling and strength constraints Compos. Struct. 7 1987 21 58
22. S.C. Tillman A finite element study of effects of connector spacing and distribution on the initial buckling stress of a twin-celled box column Thin-Walled Struct. 22 1995 1 7
23. S.P. Timoshenko, and J.N. Goodier Theory of Elasticity third ed. 1970 McGraw-Hill Singapore
24. J.M. Whitney, and R.J. Nusimer Stress fracture criteria for laminated composites containing stress concentrations J. Compos. Mater. 8 1974 253 265
25. S.E. Yamada, and C.T. Sun Analysis of laminate strength and its distribution J. Compos. Mater. 12 1978 275 284