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ZHAO Liang-yu, YANG Shu-xing, XU Yong. Uncertainty quantification for a flapping airfoil with a stochastic velocity deviation[J]. JOURNAL OF BEIJING INSTITUTE OF TECHNOLOGY, 2011, 20(3): 324-330.
Citation: ZHAO Liang-yu, YANG Shu-xing, XU Yong. Uncertainty quantification for a flapping airfoil with a stochastic velocity deviation[J].JOURNAL OF BEIJING INSTITUTE OF TECHNOLOGY, 2011, 20(3): 324-330.

Uncertainty quantification for a flapping airfoil with a stochastic velocity deviation

  • Received Date:2010-09-06
  • An outdoor flapping wing micro air vehicle (FWMAV) should be able to withstand unpredictable perturbations in the flight condition. The responses of the time-averaged thrust coefficient and the propulsive efficiency with respect to a stochastic flight velocity deviation were numerically investigated. The deviation was assumed to obey the Gauss distribution with a mean value of zero and a specified standard deviation. The probability distributions of the flapping performances were quantified by the non-intrusive polynomial chaos method. It was observed that both of the time-averaged thrust coefficient and the propulsive efficiency obeyed Gauss-like but not the exact Gauss distribution. The velocity deviation had a large effect on the time-averaged thrust coefficient and a small effect on the propulsive efficiency.
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