On a shear-deformable theory of anisotropic thin-walled beams: further contribution and validations
Source abstract
Abstract
Within the framework of an existing anisotropic thin-walled beam model, a number of non-classical effects are further incorporated and the model thereby developed is validated. Three types of lay-ups, namely, the cross-ply, circumferentially uniform stiffness, and circumferentially asymmetric stiffness are investigated. The solution methodology is based on the Extended Galerkin's Method and the non-classical effects on the static responses and natural frequencies are investigated. Comparisons of the predictions by the present model with experimental data and other analytical as well as numerical results are conducted and pertinent conclusions are drawn. This work is the first attempt to validate a class of refined thin-walled beam model that has been extensively used towards the study, among others, of dynamic response, static aeroelasticity and structural/aeroelastic feedback control.
Source: openaire · Quality: candidate unverified · Source record ↗
Research context
OpenAlex topics: Composite Structure Analysis and Optimization · Vibration and Dynamic Analysis · Aeroelasticity and Vibration Control
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
References (33)
Show source-provided references
1. Free vibration analysis of anisotropic thin-walled closed-section beams10.2514/3.12744 ↗
2. A geometrically non-linear theory for laminated anisotropic thin-walled beams10.1016/0020-7225(94)00118-4 ↗
3. Experimental–theoretical investigation of the vibration characteristics of rotating composite box beams10.2514/3.46216 ↗
4. Structural response of composite beams and blades with elastic couplings10.1016/0961-9526(92)90032-2 ↗
5. Thin-walled composite beams under bending torsional and extensional loads10.2514/3.25331 ↗
6. The influence of coupling on the free vibration of anisotropic thin-walled closed-section beams10.1016/S0020-7683(97)00365-X ↗
7. A dynamic finite element (DFE) method for free vibrations of bending–torsion coupled beams10.1016/S1270-9638(00)00114-0 ↗
8. Free-vibration analysis of composite beams10.4050/JAHS.36.36 ↗
9. Assessment of composite rotor blade modeling techniques10.4050/JAHS.44.188 ↗
10. Analysis of thick hollow composite beams under general loadings10.1016/0263-8223(95)00146-8 ↗
11. Thick-walled composite beam theory including 3-d elastic effects and torsional warping10.1016/S0020-7683(96)00072-8 ↗
12. Control of cantilevers vibration via structural tailoring and adaptive materials10.2514/2.262 ↗
13. Integrated structural tailoring and control using adaptive materials for advanced aircraft wings10.2514/3.46923 ↗
14. Refined structural modeling for enhancing vibrations and aeroelastic characteristics of composite aircraft wings
15. Dynamic response control of thin-walled beams to blast pulses using structural tailoring and piezoelectric actuation10.1115/1.2789082 ↗
16. Dynamic response of cantilevered thin-walled beams to blast and sonic-boom loadings10.1155/1998/526216 ↗
17. Behavior of thin-walled beams made of advanced composite materials and incorporating non-classical effects10.1115/1.3121352 ↗
18. On the static aeroelastic tailoring of composite aircraft swept wings modeled as thin-walled beam structures10.1016/0961-9526(92)90039-9 ↗
19. Adaptive vibrational behavior of cantilevered structures modeled as composite thin-walled beams10.1016/0020-7225(93)90123-C ↗
20. Meirovitch · 1997
21. Na SS. Control of dynamic response of thin-walled composite beams using structural tailoring and piezoelectric actuation. PhD Thesis. Virginia Polytechnic Institute and State University, 1997
22. Oscillation control of cantilevers via smart materials technology and optimal feedback control: actuator location and power consumption issues10.1088/0964-1726/7/6/011 ↗
23. Vibration and buckling characteristics of composite cylindrical panels incorporating the effects of a higher order shear theory10.1016/0020-7683(91)90198-O ↗
24. Nonclassical behavior of thin-walled composite beams with closed cross sections10.4050/JAHS.35.42 ↗
25. Aeroelastic tailoring – theory, practice and promise10.2514/3.45260 ↗
26. Formulation and evaluation of an analytical model for composite box-beams10.4050/JAHS.36.23 ↗
27. Song O. Modeling and response analysis of thin-walled beam structures constructed of advanced composite materials. PhD Thesis. Virginia Polytechnic Institute and State University, 1990
28. Dynamic response of anisotropic thin-walled beams to blast and harmonically oscillating loads10.1016/S0734-743X(98)00019-0 ↗
29. Free vibration of anisotropic composite thin-walled beams of closed cross-section contour10.1006/jsvi.1993.1325 ↗
30. Application of adaptive technology to static aeroelastic control of wing structures10.2514/3.11633 ↗
31. Higher-order shear deformation theory for thin-walled composite beams10.2514/3.47044 ↗
32. Volovoi VV, Hodges DH, Cesnik CES, Popescu B. Assessment of beam modeling methods for rotor blade applications. In: Journal of the American Helicopter Society, 55th Annual Forum, Montreal, Que., Canada, May 25–27, 1999
33. Simplified theory for composite thin-walled beams10.2514/3.11641 ↗