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Propagation of Parametric Uncertainties in a Nonlinear Aeroelastic System Using an Improved Adaptive Sparse Grid Quadrature Routine
Published in American Society of Mechanical Engineers (ASME)
2018
Volume: 4
   
Issue: 4
Abstract
A novel uncertainty quantification routine in the genre of adaptive sparse grid stochastic collocation (SC) has been proposed in this study to investigate the propagation of parametric uncertainties in a stall flutter aeroelastic system. In a hypercube stochastic domain, presence of strong nonlinearities can give way to steep solution gradients that can adversely affect the convergence of nonadaptive sparse grid collocation schemes. A new adaptive scheme is proposed here that allows for accelerated convergence by clustering more discretization points in regimes characterized by steep fronts, using hat-like basis functions with nonequidistant nodes. The proposed technique has been applied on a nonlinear stall flutter aeroelastic system to quantify the propagation of multiparametric uncertainty from both structural and aerodynamic parameters. Their relative importance on the stochastic response is presented through a sensitivity analysis. Copyright © 2018 by ASME.
About the journal
JournalASCE-ASME Journal of Risk and Uncertainty in Engineering Systems, Part B: Mechanical Engineering
PublisherAmerican Society of Mechanical Engineers (ASME)
ISSN23329017
Open AccessNo
Concepts (14)
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    Aerodynamic stalling
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    Flutter (aerodynamics)
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    Sensitivity analysis
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    STALL INDICATORS
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    Stochastic systems
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    Accelerated convergence
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    Aerodynamic parameters
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    NONLINEAR AEROELASTIC SYSTEM
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    Parametric uncertainties
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    STOCHASTIC COLLOCATION
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    Stochastic response
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    STRONG NONLINEARITY
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    Uncertainty quantifications
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    Aeroelasticity