Dynamic Response of Anisotropic Thin-walled Beams to Blast and Harmonically Oscillating Loads

International Journal of Impact Engineering

Volumn 21, Issue 8, 1998, Pages 663-682

  Song, Ohseop ^a   Ju, Joung Su ^a   Librescu, Liviu ^b  

^a Chungnam National University   (South Korea)

^b VIRGINIA POLYTECHNIC INSTITUTE AND STATE UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ANISOTROPY; BLASTING; DYNAMIC RESPONSE; ELASTICITY; MATHEMATICAL MODELS; STIFFNESS; STRUCTURAL ANALYSIS; STRUCTURAL LOADS;

BENDING-TWIST ELASTIC COUPLING;

BEAMS AND GIRDERS;

EID: 0032155305     PISSN: 0734743X     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0734-743X(98)00019-0     Document Type: Article

References (16)

1. I. L. Librescu and A. Nosier, Dynamic response of anisotropic composite panels to time-dependent external excitations. Paper ICAS-90-1.4R, 17th Congress of the International Council of the Aeronautical Sciences, September, 2134-2144 (1990). Stockholm Sweden.
2. O. Song and L. Librescu, Bending vibration of cantilevered thin-walled beams subjected to time-dependent external excitations. J. Acoust. Soc. Amer. 98(1), 313-319 (1995).
3. L. Librescu and O. Song, On the static aeroelastic tailoring of composite aircraft swept wings modelled as thin-walled beam structures. Composites Engng. 2 (5-7) 497-512 (1992).
4. O. Song and L. Librescu, Free vibration of anisotropic composite thin-walled beams of closed cross-section contour, J. Sound Vibration 167 (1), 129-147 (1993).
5. L. Librescu and S. Thangjitham, Analytical studies on static aeroelastic characteristics for composite forward-swept wing aircraft. J. Aircraft 28 (2), 157-167 (1991).
6. L. Librescu, L. Meirovitch and O. Song, Refined structural modeling for enhancing vibrational and aeroelastic characteristics of composite aircraft wings. La Recherche Aerospatiale, 1, 23-25 (1996).
7. L. W. Rehfield, A. R. Atilgan and D. H. Hodges, Nonclassical behavior of thin-walled composite beams with closed cross sections. J. Amer. Helicopter Soc. 35 (2), 42-50 (1990).
8. L. W. Rehfield and A. R. Atilgan. Toward understanding the tailoring mechanisms for thin-walled composite tubular beams. Proc. 1st USSR-USA Symp on Mechanics of Composite Materials, Riga, Latvia, USSR, 1989, 23-26 May (Eds) S. W. Tsai, J. M. Whitney, T. W. Chou and R. M. Jones, ASME, 187-196 (1989).
9. E. C. Smith and I. Chopra, Formulation and evaluation of an analytical model for composite box-beams. J. Amer. Helicopter Soc. 36 (3), 36-47 (1991).
10. L. Librescu, Elastostatics and Kinetics of Anisotropic and Heterogeneous Shell-Type Structures. Noordhoff International Publishers, Leyden, The Netherlands (1975).
11. A. L. Dobyns, Analysis of simply-supported orthotropic plates subject to static and dynamic loads." AIAA J. 19, 642-650 (1981).
12. V. Birman and C. W. Bert, Behavior of laminated plates subjected to conventional blast. Int. J. Impact Engng. 6 (3) 145-155 (1987).
13. K. R. V. Kaza and R. E. Kielb, Effects of warping and pretwist on torsional vibration of rotating beams. J. Appl. Mech. 23 (6) (1987).
14. G. Karpouzian and L. Librescu, Three-dimensional flutter solution of aircraft wings composed of advances composite materials, Paper AIAA-94-1490 (P. 35th Structures, Structural Dynamics and Materials Conference, pp. 2851-2856, Hilton Head, SC April 18-20 (1994).
15. L. Librescu, L. Meirovitch and S. S. Na, Control of cantilevers vibration via structural tailoring and adaptive materials. AIAA J. 35 (8) 1309-1315 (1997).
16. A. Gjelsvik, The Theory of Thin-Walled Bars. Wiley, New York (1981).