General perspectives on model construction and evaluation for stochastic estimation, with application to a blunt trailing edge wake

被引:0
|
作者
H. Clark
A. Naghib-Lahouti
P. Lavoie
机构
[1] University of Toronto,Institute for Aerospace Studies
来源
Experiments in Fluids | 2014年 / 55卷
关键词
Vortex; Variance Inflation Factor; Proper Orthogonal Decomposition; Pressure Fluctuation; Model Construction;
D O I
暂无
中图分类号
学科分类号
摘要
The technique of stochastic estimation is examined as a specific application of linear least squares modelling. Factors that are relevant to the objectives of estimation in fluids, such as the number of sensors, the use of multiple time lags, and the strength of linear correlations, are discussed in the context of a general regression formulation. We consolidate the established findings of several research fields in order to outline clearly the potential pitfalls and reasonable performance expectations of these empirical strategies. Experimental measurements of velocity and fluctuating pressure in the wake of a blunt trailing edge body are used for quantitative illustration of key considerations for model construction and performance evaluation. It is emphasized that estimator accuracy is influenced strongly by the physical relationships among the measured variables, in addition to their correlation with the estimated variable. The evaluation of several performance metrics on an independent test set provides valuable information for the selection of a suitably complex model. In particular, “variance inflation” is interpreted as an indicator of the potential amplification of noise by a stochastic estimator.
引用
收藏
相关论文
共 50 条
  • [1] General perspectives on model construction and evaluation for stochastic estimation, with application to a blunt trailing edge wake
    Clark, H.
    Naghib-Lahouti, A.
    Lavoie, P.
    EXPERIMENTS IN FLUIDS, 2014, 55 (07)
  • [2] Spanwise vortex dislocation in the wake of segmented blunt trailing edge
    Deshpande, P. J.
    Sharma, S. D.
    JOURNAL OF FLUIDS AND STRUCTURES, 2012, 34 : 202 - 217
  • [3] On wake response to asymmetric blowing in spurts from a blunt trailing edge
    Sharma, S. D.
    Pant, R. R.
    SADHANA-ACADEMY PROCEEDINGS IN ENGINEERING SCIENCES, 2007, 32 (1-2): : 111 - 122
  • [4] COHERENT STRUCTURES IN THE NEAR WAKE OF A BLUNT TRAILING EDGE PROFILED BODY
    Doddipatla, Lakshmana Sampat
    Lahouthi, Arash Naghib
    Hangan, Horia
    Siddiqqui, Kamran
    PROCEEDINGS OF THE ASME FLUIDS ENGINEERING DIVISION SUMMER CONFERENCE - 2010 - VOL 1, PTS A-C, 2010, : 2061 - 2069
  • [5] ASYMPTOTIC WAKE BEHAVIOR OF SWEPT, BLUNT TRAILING-EDGE AIRFOILS
    SELBY, GV
    MIANDOAB, FH
    JOURNAL OF FLUIDS ENGINEERING-TRANSACTIONS OF THE ASME, 1994, 116 (01): : 171 - 174
  • [6] On wake response to asymmetric blowing in spurts from a blunt trailing edge
    S. D. Sharma
    R. R. Pant
    Sadhana, 2007, 32 : 111 - 122
  • [7] Three-dimensional wake dynamics of a blunt and divergent trailing edge airfoil
    El-Gammal, M.
    Hangan, H.
    EXPERIMENTS IN FLUIDS, 2008, 44 (05) : 705 - 717
  • [8] Three-dimensional wake dynamics of a blunt and divergent trailing edge airfoil
    M. El-Gammal
    H. Hangan
    Experiments in Fluids, 2008, 44 : 705 - 717
  • [9] Wake instabilities of a blunt trailing edge profiled body at intermediate Reynolds numbers
    Naghib-Lahouti, A.
    Lavoie, P.
    Hangan, H.
    EXPERIMENTS IN FLUIDS, 2014, 55 (07)
  • [10] On experimental sensitivity analysis of the turbulent wake from an axisymmetric blunt trailing edge
    Grandemange, M.
    Gohlke, M.
    Parezanovic, V.
    Cadot, O.
    PHYSICS OF FLUIDS, 2012, 24 (03)