Study of constrained layer damping models under clamped boundary conditions

American Society of Mechanical Engineers, Aerospace Division (Publication) AD

Volumn 59, Issue , 1999, Pages 381-386

  Huang, Peter Y H ^a   Reinhall, Per G ^a   Shen, I Y ^a  

^a UNIVERSITY OF WASHINGTON   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC VARIABLES CONTROL; BOUNDARY CONDITIONS; DAMPING; DEFORMATION; FREQUENCIES; VIBRATION CONTROL; VISCOELASTICITY;

CONSTRAINED LAYER DAMPING; MEAD-MARKUS FORMULATION; MEAD-MARKUS MODEL;

CANTILEVER BEAMS;

EID: 0033293931     PISSN: 07334230     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Article

References (11)

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3. Mead, D. J., 1965, "The Effect of Certain Damping Treatment on the Response of Idealized Aeroplane Structures Excited by Noise," Air Force Materials Lab., AFML-TR-65-284 WPAFB.
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6. Rao, D. K., 1978, "Frequency and Loss Factors of Sandwich Beams under Various Boundary Conditions," Journal Mechanical Engineering Science, Vol. 20 No. 5, pp. 271-282.
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8. Shen, I. Y., 1994, "Hybrid Damping Through Intelligent Constrained Layer Treatments," ASME Journal of Vibration and Acoustics, Vol. 116, pp. 341-349.
9. Soovere, J. and Drake, M. L., 1985, Aerospace Structures Technology Damping Design Guide Vol. III - Damping Material Data, AF Wright Aeronautical Laboratories, Ohio.
10. Swallow. W., 1939, "An Improved Method of Damping Panel Vibrations," British Patent Specification 513, 171.
11. Yang, B. and Tan, C. A., 1992, "Transfer Function of One-Dimensional Distributed Parameter System," ASME Journal of Applied Mechanics, Vol. 59, pp. 1009-1014.