Surrogate-based aeroelastic loads prediction in the presence of shock-induced separation

被引:16
作者
Brouwer, Kirk R. [1 ]
McNamara, Jack J. [1 ]
机构
[1] Ohio State Univ, Dept Mech & Aerosp Engn, Columbus, OH 43210 USA
关键词
Surrogate models; Kriging; NARX model; Panel flutter; Limit cycle oscillation; Supersonic; Shock impingement; Two-dimensional; UNSTEADY AERODYNAMICS; VOLTERRA THEORY; PISTON THEORY; FLUTTER; OSCILLATIONS; STABILITY; PROGRESS; PANEL;
D O I
10.1016/j.jfluidstructs.2019.102838
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
A surrogate-based modeling strategy is presented for robust and efficient prediction of unsteady aeroelastic loads in the presence of shock-induced separation. Enriched piston theory predictions are extended with a data-driven nonlinear autoregressive with exogenous inputs model to account for hysteresis from the interplay of a dynamically deforming surface with the separation bubble in a shock/boundary layer interaction. The approach is evaluated for prescribed surface motion and shock-induced panel flutter responses, with good agreement observed in each scenario relative to unsteady Reynolds-averaged Navier-Stokes simulations. For the latter, excellent agreement is observed in the prediction of the stability boundary and oscillation frequency. In contrast, the oscillation amplitude conservatively deviates from the Reynolds-averaged Navier-Stokes solution with increasing dynamic pressure. The online computational cost of the extended approach is orders of magnitude less than that required for predictions using an unsteady Reynolds-averaged Navier-Stokes model. (C) 2019 Published by Elsevier Ltd.
引用
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页数:20
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