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    A Resonant Beam Tuned Damping Device 

    Source: Journal of Engineering for Gas Turbines and Power:;1969:;volume( 091 ):;issue: 003:;page 143
    Author(s): A. D. Nashif; D. I. G. Jones
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A resonant beam tuned damping device, comprising a flexible beam joined by way of visco-elastic links at the ends, to a vibrating structure, is described. This device has the advantage of ...
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    The Effect of Stringer Width and Damping on the Response of Skin—Stringer Structures 

    Source: Journal of Manufacturing Science and Engineering:;1972:;volume( 094 ):;issue: 001:;page 159
    Author(s): J. P. Henderson; A. D. Nashif
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Analytical and experimental results for a five-span skin-stringer structure are presented. The analysis uses a transfer matrix technique which considers the effects of stringer dimensions including ...
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    Vibrating Beam Dampers for Reducing Vibrations in Gas Turbine Blades 

    Source: Journal of Engineering for Gas Turbines and Power:;1975:;volume( 097 ):;issue: 001:;page 111
    Author(s): D. I. G. Jones; A. D. Nashif; H. Stargardter
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper reports the results of a preliminary investigation of the feasibility of reducing vibratory response levels in jet engine turbine blades by means of tuned damping devices incorporating ...
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    Vibration Damping 

    Source: Journal of Vibration and Acoustics:;1987:;volume( 109 ):;issue: 001:;page 124
    Author(s): A. D. Nashif; H. Saunders; D. I. G. Jones; J. P. Henderson
    Publisher: The American Society of Mechanical Engineers (ASME)
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