Similarities between solid and thin-walled composite beams by analytic approach

Journal of Aircraft

Volumn 35, Issue 4, 1998, Pages 604-615

  Rand, Omri ^a,b  

^a TECHNION ISRAEL INSTITUTE OF TECHNOLOGY   (Israel)

^b Faculty of Aerospace Engineering   (Israel)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT MATERIALS; AIRCRAFT PARTS AND EQUIPMENT; COMPOSITE STRUCTURES; FINITE DIFFERENCE METHOD; MATHEMATICAL MODELS; NUMERICAL ANALYSIS; SHEAR DEFORMATION; STRESSES; STRUCTURAL LOADS;

COMPOSITE BEAMS; LAMINATED BEAMS;

LAMINATED COMPOSITES;

EID: 0032117161     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/2.2344     Document Type: Article

References (32)

1. Bull, J. W. (ed.), "Numerical Analysis and Modelling of Composite Materials," Analysis of Composite Rotor Blades, Chapman & Hall, London, Dec. 1995, Chap. 1.
2. Hong, C. H., and Chopra, I., "Aeroelastic Stability of a Composite Blade," Journal of the American Helicopter Society, Vol. 30, No. 2, 1985, pp. 57-67.
3. Yuan, K., Friedmann, P. P., and Venkatesan, C., "Aeroelastic Behavior of Composite Rotor Blades with Swept Tips," Proceedings of the American Helicopter Society 48th Annual Forum (Washington, DC), American Helicopter Society, Alexandria, VA, 1992, pp. 1039-1059.
4. Morison, W. D., "The Effect of Moisture Loss and Elevated Temperature upon the Material Damping of Fiber Reinforced Polymer Matrix Composites," Univ. of Toronto Inst. for Aerospace Studies (UTIAS), Rept. 324, Toronto, Canada, July 1988.
5. Llanos, A. S., Lucchetto, L. A., Stafford, D., and Coulliette, C., "Environmental Conditions for Certification Testing of Helicopter Advanced Composite Main Rotor Components," 48th Annual Forum of the American Helicopter Society, Washington, DC, June 1992.
6. Liu, S., Kutlu, Z., and Chang, F. K., "Matrix Cracking and Delamination in Laminated Composite Beams Subjected to a Transverse Concentrated Line Load," Journal of Composite Materials, Vol. 27, No. 5, 1993, pp. 436-470.
7. Noor, A. K., and Burton, W. S., "Assessment of Shear Deformation Theories for Multilayered Composite Plates," Applied Mechanics Reviews, Vol. 42, No. 1, 1989, pp. 1-13.
8. Gordaninejad, F., and Ghazavi, A., "Effect of Shear Deformation on Bending of Laminated Composite Beams," Journal of Pressure Vessel Technology, Transactions of the ASME, Vol. 111, No. 2, 1989, pp. 159-164.
9. Nosier, A., and Reddy, J. N., "On Vibration and Buckling of Symmetric Laminated Plates According to Shear Deformation Theories," Acta Mechanica, Vol. 94, No. 3-4, 1992, pp. 123-169.
10. Maiti, D. K., and Sinha, P. K., "Bending and Free Vibration Analysis of Shear Deformable Laminated Composite Beams by Finite Element Methods," Journal of Composite Structures, Vol. 29, No. 1, 1994, pp. 421-431.
11. Zapfe, J. A., and Lesieutre, G. A., "Iterative Calculation of the Transverse Shear Distribution in Laminated Composite Beams," Proceedings of the AIAA/ASME/ASCE/AHS/ASC 36th Structures, Structural Dynamics, and Materials Conference and AIAA/ASME Adaptive Structures Forum (New Orleans, LA), AIAA, Washington, DC, 1995, pp. 3117-3125.
12. Wang, S. S., and Choi, I., "Boundary-Layer Effects in Composite Laminates: Part 1-Free Edge Stress Singularities," Journal of Applied Mechanics, Vol. 49, No. 1, 1982, pp. 541-548.
13. Wang, S. S., and Choi, I., "Boundary-Layer Effects in Composite Laminates: Part 2-Free Edge Stress Solutions and Basic Characteristics," Journal of Applied Mechanics, Vol. 49, No. 1, 1982, pp. 549-560.
14. Rand, O., "Interlaminar Shear Stresses in Solid Composite Beams Using a Complete Shear Deformation Model," AIAA/ASME/ASCE/ AHS/ASC 37th Structures, Structural Dynamics, and Materials Conf., Salt Lake City, UT, April 1996.
15. Kosmatka, J. B., and Friedmann, P. P., "Structural Dynamic Modeling of Advanced Composite Propellers by the Finite Element Method," Proceedings of the AIAA/ASME/ASCE/AHS 28th Structures, Structural Dynamics, and Materials Conference (Monterey, CA), AIAA, Washington, DC, 1987, pp. 111-124.
16. Kosmatka, J. B., and Friedmann, P. P., "Vibration Analysis of Composite Turbopropellers Using a Nonlinear Beam-Type Finite Element Approach," AIAA Journal, Vol. 27, No. 11, 1989, pp. 1606-1614.
17. Stemple, A. D., and Lee, S. W., "A Finite Element Model for Composite Beams Undergoing Large Deflections with Arbitrary Cross Sectional Warping." international Journal for Numerical Methods in Engineering, Vol. 28. No. 9, 1989, pp. 2143-2163.
18. Giavotto, V., Borri, M., Mantegazza, P., Ghiringhelli, G., Carmaschi, V., Maffioli, G. C., and Mussi, F., "Anisotropic Beam Theory and Applications," Computers and Structures, Vol. 16, Nos. 1-4, 1983, pp. 403-413.
19. Perngjin, F. P., and Nayfeh, A. H., "A Fully Nonlinear Theory of Curved and Twisted Composite Rotor Blades Accounting for Warping and Three-Dimensional Stress Effects," International Journal of Solids and Structures, Vol. 31, No. 9, 1994, pp. 1309-1340.
20. Fish, J. C., "Stress Analysis of Composite Rotor Systems," 47th Annual Forum of the American Helicopter Society, Phoenix, AZ, May 1991.
21. Kalfon, J. P., and Rand, O., "Nonlinear Analysis of Composite Thin-Walled Helicopter Blades," Journal of Computers and Structures, Vol. 48, No. 1, 1993, pp. 51-61.
22. Rand, O., "Nonlinear Analysis of Orthotropic Beams of Solid Cross-Sections," Journal of Composite Structures, Vol. 29, No. 1, 1994, pp. 27-45.
23. Minguet, P., and Dugundji, J., "Experiments and Analysis for Composite Blades Under Large Deflections, Part I: Static Behavior," AIAA Journal, Vol. 28, No. 9, 1990, pp. 1573-1579.
24. Minguet, P., and Dugundji, J., "Experiments and Analysis for Composite Blades Under Large Deflections, Part II: Dynamic Behavior," AIAA Journal, Vol. 28, No. 9, 1990, pp. 1580-1588.
25. Chandra, R., Stemple, A. D., and Chopra, I., Thin-Walled Composite Beams Under Bending, Torsional, and Extensional Loads," Journal of Aircraft, Vol. 27, No, 7, 1990, pp. 619-626.
26. Chandra, R., and Chopra, I., "Vibration Characteristics of Composite I-Beam with Elastic Couplings Under Rotation," 47th Annual Forum of the American Helicopter Society, Phoenix, AZ, May 1991.
27. Berdichevsky, E. A., Armanios, E., and Ashraf, B., "Theory of Anisotropic Thin-Walled Closed-Cross-Section Beams," Composite Engineering, Vol. 2, Nos. 5-7, 1992, pp. 411-432.
28. Rand, O., and Barkai, S. M., "Analytic Insight into the Structural Couplings and Nonlinear Formulation of Solid and Thin-Walled Composite Blades," American Helicopter Society 52nd Annual Forum, Washington, DC, June 1996.
29. Timoshenko, S. P., and Goodier, J. N., Theory of Elasticity, 3rd ed., McGraw-Hill, New York, 1970.
30. Ochoa, O. O., and Reddy, J. N., Finite Element Analysis of Composite Laminates, Kluwer, Dordrecht, The Netherlands, 1992.
31. Sun, C. T., and Li, S., "Three-Dimensional Effective Elastic Constants for Thick Laminates," Journal of Composite Materials, Vol. 22, No. 7, 1988, pp. 629-639.
32. Sokolnikoff, I. S., Mathematical Theory of Elasticity, 2nd ed., McGraw-Hill, New York, 1956.