CHARACTERIZING THE DYNAMIC RESPONSE OF A THERMALLY LOADED, ACOUSTICALLY EXCITED PLATE

In this work the dynamic response is considered of a homogeneous, fully clamped rectangular plate subject to spatially uniform thermal loads and narrow-band acoustic excitation. In both the pre-and post-buckled regimes, the small amplitude, linear response is confirmed. However, the primary focus is...

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Published inJournal of sound and vibration Vol. 196; no. 5; pp. 635 - 658
Main Authors Murphy, K.D., Virgin, L.N., Rizzi, S.A.
Format Journal Article
LanguageEnglish
Published London Elsevier Ltd 10.10.1996
Elsevier
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ISSN0022-460X
1095-8568
DOI10.1006/jsvi.1996.0506

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Abstract In this work the dynamic response is considered of a homogeneous, fully clamped rectangular plate subject to spatially uniform thermal loads and narrow-band acoustic excitation. In both the pre-and post-buckled regimes, the small amplitude, linear response is confirmed. However, the primary focus is on the large amplitude, non-linear, snap-through response, because of the obvious implications for fatigue in aircraft components. A theoretical model is developed which uses nine spatial modes and incorporates initial imperfections and non-ideal boundary conditions. Because of the higher order nature of this model, it is inherently more complicated than a one-mode buckled beam equation (Duffing's equation). An experimental system was developed to complement the theoretical results, and also to measure certain system parameters for the model which are not available theoretically. Several analysis techniques are used to characterize the response. These include time series, power spectra and autocorrelation functions. In addition, the fractal dimension and Lyapunov exponents for the response are computed to address the issue of spatial dimension and temporal complexity (chaos), respectively. Comparisons between theory and experiment are made and show considerable agreement. However, these comparisons also serve to point out difficulties in computing the fractal dimension and Lyapunov exponents from experimental data.
AbstractList In this work the dynamic response is considered of a homogeneous, fully clamped rectangular plate subject to spatially uniform thermal loads and narrow-band acoustic excitation. In both the pre-and post-buckled regimes, the small amplitude, linear response is confirmed. However, the primary focus is on the large amplitude, non-linear, snap-through response, because of the obvious implications for fatigue in aircraft components. A theoretical model is developed which uses nine spatial modes and incorporates initial imperfections and non-ideal boundary conditions. Because of the higher order nature of this model, it is inherently more complicated than a one-mode buckled beam equation (Duffing's equation). An experimental system was developed to complement the theoretical results, and also to measure certain system parameters for the model which are not available theoretically. Several analysis techniques are used to characterize the response. These include time series, power spectra and autocorrelation functions. In addition, the fractal dimension and Lyapunov exponents for the response are computed to address the issue of spatial dimension and temporal complexity (chaos), respectively. Comparisons between theory and experiment are made and show considerable agreement. However, these comparisons also serve to point out difficulties in computing the fractal dimension and Lyapunov exponents from experimental data.
Author Murphy, K.D.
Rizzi, S.A.
Virgin, L.N.
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  fullname: Rizzi, S.A.
  organization: NASA Langley Research Center, Structural Acoustics Branch, Hampton, VA 23681-0001, U.S.A
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Issue 5
Keywords Dynamic response
Acoustic wave
Fatigue
Dynamic loads
Numerical method
Thermal load
Experimental study
Narrow band
Fractal
Dynamic stability
Testing equipment
Rectangular plate
Non linear effect
Aircraft
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StartPage 635
SubjectTerms Acoustics
Exact sciences and technology
Fundamental areas of phenomenology (including applications)
Physics
Solid mechanics
Structural acoustics and vibration
Structural and continuum mechanics
Vibration, mechanical wave, dynamic stability (aeroelasticity, vibration control...)
Vibrations and mechanical waves
Title CHARACTERIZING THE DYNAMIC RESPONSE OF A THERMALLY LOADED, ACOUSTICALLY EXCITED PLATE
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