Dynamic Stability of a Composite Circular Cylindrical Shell Subjected to Combined Axial and Torsional Loading
dc.contributor.author | Argento, A. | en_US |
dc.date.accessioned | 2010-04-13T18:56:10Z | |
dc.date.available | 2010-04-13T18:56:10Z | |
dc.date.issued | 1993 | en_US |
dc.identifier.citation | Argento, A. (1993). "Dynamic Stability of a Composite Circular Cylindrical Shell Subjected to Combined Axial and Torsional Loading." Journal of Composite Materials 27(18): 1722-1738. <http://hdl.handle.net/2027.42/66879> | en_US |
dc.identifier.issn | 0021-9983 | en_US |
dc.identifier.uri | https://hdl.handle.net/2027.42/66879 | |
dc.description.abstract | The dynamic stability of thin, clamped, composite circular cylindrical shells is studied for combined axial and torsional loading. Each load is taken to be har monically varying; the frequencies of the two loads differ, in general. For the case in which the frequencies are commensurate, the applied load function is periodic. The equa tions of motion for the shell are reduced to a system of Hill equations by means of Fourier series expansions. Instability regions of principal and combination parametric resonance are determined by use of the monodromy matrix. Numerical results are generated for boron-epoxy layered shells for various cases of pure axial, pure torsional, and combined loading. The width of the principal instability region is presented as a function of fiber ori entation for a laminate case. Stability diagrams are presented covering about 6 times the lowest natural frequency for various ratios of the applied axial and torsional frequencies. | en_US |
dc.format.extent | 3108 bytes | |
dc.format.extent | 539365 bytes | |
dc.format.mimetype | text/plain | |
dc.format.mimetype | application/pdf | |
dc.publisher | Sage Publications | en_US |
dc.subject.other | Dynamic Stability | en_US |
dc.subject.other | Shell | en_US |
dc.subject.other | Composite | en_US |
dc.subject.other | Parametric Resonance. | en_US |
dc.title | Dynamic Stability of a Composite Circular Cylindrical Shell Subjected to Combined Axial and Torsional Loading | en_US |
dc.type | Article | en_US |
dc.subject.hlbsecondlevel | Aerospace Engineering | en_US |
dc.subject.hlbtoplevel | Engineering | en_US |
dc.description.peerreviewed | Peer Reviewed | en_US |
dc.contributor.affiliationum | Department of Mechanical Engineering University of Michigan-Dearborn4901 Evergreen Road Dearborn, MI48128-1491 | en_US |
dc.description.bitstreamurl | http://deepblue.lib.umich.edu/bitstream/2027.42/66879/2/10.1177_002199839302701802.pdf | |
dc.identifier.doi | 10.1177/002199839302701802 | en_US |
dc.identifier.source | Journal of Composite Materials | en_US |
dc.identifier.citedreference | Srinivasan, R.S. and P. Chellapandi 1986 "Dynamic Stability of Rectangular Laminated Composite Plates," Computers and Structures, 24 233-238 | en_US |
dc.identifier.citedreference | Tylikowski, A. 1989 "Dynamic Stability of Nonlinear Antisymmetrically-Laminated Cross-Ply Rectangular Plates," American Society of Mechanical Engineers Journal of Applied Mechanics, 56 375-381 | en_US |
dc.identifier.citedreference | Librescu, L. and S. Thangjitham 1990 "Parametric Instability of Laminated Composite Shear Deformable Flat Panels Subjected to In-Plane Edge Loads," Int. J Non-Linear Mechanics, 25:263-273 | en_US |
dc.identifier.citedreference | Bert, C.W. and V. Birman. 1987. "Dynamic Instability of Shear Deformable Antisymmetric Angle-Ply Plates," Int. J. Solids Structures, 23:1053-1061 | en_US |
dc.identifier.citedreference | Moorthy, J., J.N. Reddy and R.H. Plaut. 1990. "Parametric Instability of Laminated Composite Plates with Transverse Shear Deformation," Int. J. Solids Structures, 26.801-811 | en_US |
dc.identifier.citedreference | . Bert, C.W. and V. Birman. 1988. "Parametric Instability of Thick Orthotropic, Circular Cylindrical Shells," Acta Mechanica, 71:61-76 | en_US |
dc.identifier.citedreference | . Argento, A. and R.A. Scott. 1989. "Parametric Resonance of Arbitrarily Layered Fiber Reinforced Composite Circular Cylindrical Shells," Proceedings of the 4th Technical Conference of the American Society of Composites, pp 649-656 | en_US |
dc.identifier.citedreference | . Argento, A. and R.A. Scott. 1993. "Dynamic Instability of Layered Anisotropic Circular Cylindrical Shells, Part I: Theoretical Development," Journal of Sound and Vibration, 162:311-322 | en_US |
dc.identifier.citedreference | . Argento, A. and R.A. Scott 1993. "Dynamic Instability of Layered Anisotropic Circular Cylindrical Shells, Part 2: Numerical Results," Journal of Sound and Vibration, 162.323-332 | en_US |
dc.identifier.citedreference | Goroshko, O.A. and V.V. Emel'yanenko. 1975. "Dynamic Stability of Layered Anisotropic Shells," Soviet Applied Mechanics. UDC539.3:534.1, pp. 720-725 | en_US |
dc.identifier.citedreference | . Stuart, R.J., S. Dharmarajan and L.E. Penzes. 1980. "Dynamic Stability of Fibrous Composite Cylinders," in Fibrous Composites in Structural Design New York: Plenum Press, pp. 329-340 | en_US |
dc.identifier.citedreference | Aida, T. 1989 "Dynamic Stability of Thin-Walled Structural Members under Periodic Axial Torque," ASCE Journal of Engineering Mechanics, 115:71-88 | en_US |
dc.identifier.citedreference | Plaut, R.H., J.J. Gentry and D.T. Mook. 1990. "Non-Linear Structural Vibrations under Combined Multi-Frequency Parametric and External Excitations," Journal of Sound and Vibration, 140.381-390 | en_US |
dc.identifier.citedreference | . Brush, D.O. and B.O. Almroth 1975. Buckling of Bars, Plates, and Shells New York Mc Graw-Hill. | en_US |
dc.identifier.citedreference | Whitney, J.M. and C.T. Sun 1975. "Buckling of Composite Cylindrical Characterization Specimens," J Composite Materials, 9 138-148 | en_US |
dc.identifier.citedreference | Bolotin, V.V. 1964 The Dynamic Stability of Elastic Systems San Francisco: Holden-Day | en_US |
dc.identifier.citedreference | Meirovitch, L. 1970. Methods of Analytical Dynamics New York Mc Graw-Hill. | en_US |
dc.identifier.citedreference | von Kerczek, C. and S.H. Davis. 1975. "Calculation of Transition Matrices," AIAA Journal, 13:1400-1403 | en_US |
dc.identifier.citedreference | . Gaonkar, G.H., D.S. Simha Prasad and D. Sastry 1981. "On Computing Floquet Transition Matrices of Rotorcraft," Journal of the American Helicopter Society, 26 56-61. | en_US |
dc.owningcollname | Interdisciplinary and Peer-Reviewed |
Files in this item
Remediation of Harmful Language
The University of Michigan Library aims to describe library materials in a way that respects the people and communities who create, use, and are represented in our collections. Report harmful or offensive language in catalog records, finding aids, or elsewhere in our collections anonymously through our metadata feedback form. More information at Remediation of Harmful Language.
Accessibility
If you are unable to use this file in its current format, please select the Contact Us link and we can modify it to make it more accessible to you.