TECHNICAL PAPERS
Oct 1, 1994

Continuous Dynamic Model for Tapered Beam‐Like Structures

Publication: Journal of Aerospace Engineering
Volume 7, Issue 4

Abstract

Distributed parameter modeling may offer a viable alternative to the finite‐element approach for modeling large flexible space structures. In addition, the introduction of the transfer matrix method to the continuum modeling process provides a very useful tool to facilitate the distributed parameter model applied to more complex configurations. This paper proposes a piecewise continuous Timoshenko beam model, which was used for the dynamic analysis of a tapered beam‐like structure. Instead of the arbitrarily assumed shape functions used in a finite‐element analysis, the closed‐form solution of the Timoshenko beam equation was used. Application of the transfer matrix method was used to relate all elements as a whole. Using the corresponding boundary conditions and compatibility equations, a characteristic equation for the global tapered beam was produced and natural frequencies derived. The results from this analysis were compared to those obtained from a conventional finite‐element analysis. While comparable results are obtained, the piecewise continuous Timoshenko beam model significantly decreased the number of modal elements required.

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References

1.
Balakrishnan, A. V. (1985). “A mathematical formulation of the SCOPE problem: Part I.” NASA CR 172581, University of California at Los Angeles, Calif.
2.
Taylor Jr., L. W., and Williams, J. (1988). “Maximum likelihood estimation for distributed parameter models of flexible spacecraft.” IFAC/IFORS Symp. on Identification and Parameter Estimation, Beijing, China.
3.
Shen, J. Y., Huang, J. K., and Taylor Jr., L. W. (1992). “Likelihood estimation for distributed parameter models of large beam‐like structures.” J. Sound and Vibration, 155(3), 467–480.
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Thomas, S. (1989). “A continuum model for dynamic analysis of the space station.” 40th IAF Int. Astronautical Cong., Malaga, Spain.
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Shen, J. Y., and Taylor Jr., L. W. (1992). “Application of transfer matrix method to estimate the modal characteristics of the NASA mini‐mast truss.” NASA Workshop on Distributed Parameter Modeling and Control of Flexible Aerosp. Systems, Williamsburg, Va., NASA Cp‐3242, 77–94.
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Taylor Jr., L. W., Shen, J. Y., and Sharpe Jr., L. (1993). “Applying transfer matrix method to formulate a distributed parameter model for the LACE satellite model.” 9th VPI&SU Symp. on Dynamic & Control of Large Space Struct., Virginia Polytechnic Institute & State University, Blacksburg, Va., 13–24.
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Shen, J. Y., Huang, J. K., and Taylor Jr., L. W. (1992). “Damping models for distributed parameter estimation of large beam‐like structures.” Pacific‐Rim Int. Conf. on Modelling, Simulation, and Identification, Vancouver, Canada, 171–174.
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Shen, J. Y. (1991). “Maximum likelihood estimation for distributed parameter models of large beam‐like structures,” PhD Dissertation, Dept. of Mech. Engrg. & Mech., Old Dominion University, Norfolk, Va.

Information & Authors

Information

Published In

Go to Journal of Aerospace Engineering
Journal of Aerospace Engineering
Volume 7Issue 4October 1994
Pages: 435 - 445

History

Received: Jun 28, 1993
Published online: Oct 1, 1994
Published in print: Oct 1994

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Authors

Affiliations

Ji Yao Shen
Asst. Prof., Ctr. for Aerosp. Res., School of Engrg., NC A&T State Univ., Greensboro, NC 27411
Elias G. Abu‐Saba
Prof., Dept. of Architectural Engrg., NC A&T State University, Greensboro, NC
William M. McGinley
Assoc. Prof., Dept. of Architectural Engrg., NC A&T State University, Greensboro, NC
Lonnie Sharpe, Jr.
Assoc. Prof., Dept. of Mech. Engrg., NC A&T State University, Greensboro, NC
Lawrence W. Taylor, Jr.
Chf. Sci., Control & Guidance Div., Langley Research Center, Hampton, VA 23665

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