On spectral linear stochastic estimation

An extension to classical stochastic estimation techniques is presented, following the formulations of Ewing and Citriniti (1999), whereby spectral based estimation coefficients are derived from the cross spectral relationship between unconditional and conditional events. This is essential where accurate modeling using conditional estimation techniques are considered. The necessity for this approach stems from instances where the conditional estimates are generated from unconditional sources that do not share the same grid subset, or possess different spectral behaviors than the conditional events. In order to filter out incoherent noise from coherent sources, the coherence spectra is employed, and the spectral estimation coefficients are only determined when a threshold value is achieved. A demonstration of the technique is performed using surveys of the dynamic pressure field surrounding a Mach 0.30 and 0.60 axisymmetric jet as the unconditional events, to estimate a combination of turbulent velocity and turbulent pressure signatures as the conditional events. The estimation of the turbulent velocity shows the persistence of compact counter-rotating eddies that grow with quasi-periodic spacing as they convect downstream. These events eventually extend radially past the jet axis where the potential core is known to collapse.

[1]  J. Borée,et al.  Extended proper orthogonal decomposition: a tool to analyse correlated events in turbulent flows , 2003 .

[2]  Mohammad Maqusi,et al.  Applied Time Series Analysis, Vol. 1 , 1981, IEEE Transactions on Systems, Man, and Cybernetics.

[3]  S. Lang,et al.  An Introduction to Fourier Analysis and Generalised Functions , 1959 .

[4]  Nathan E. Murray,et al.  Estimation of the flowfield from surface pressure measurements in an open cavity , 2003 .

[5]  C. Tinney Low-dimensional techniques for sound source identification in high speed jets , 2005 .

[6]  William K. George,et al.  Reconstruction of the global velocity field in the axisymmetric mixing layer utilizing the proper orthogonal decomposition , 2000, Journal of Fluid Mechanics.

[7]  Ronald Adrian,et al.  On the role of conditional averages in turbulence theory. , 1975 .

[8]  W. George,et al.  Application of a ''slice'' proper orthogonal decomposition to the far field of an axisymmetric turbulent jet , 2002 .

[9]  M. Glauser,et al.  The proper orthogonal decomposition of pressure fluctuations surrounding a turbulent jet , 1997, Journal of Fluid Mechanics.

[10]  William K. George,et al.  Downstream evolution of the most energetic modes in a turbulent axisymmetric jet at high Reynolds number. Part 1. The near-field region , 2004, Journal of Fluid Mechanics.

[11]  J. Landes Application of a J-Q Model for Fracture in the Ductile-Brittle Transition , 1997 .

[12]  Charles E. Tinney,et al.  Spatial Correlations in a Transonic Jet , 2007 .

[13]  Joseph H. Citriniti,et al.  Examination of a LSE/POD complementary technique using single and multi-time information in the axisymmetric shear layer , 1999 .

[14]  M. Glauser,et al.  The Evolution of the Most Energetic Modes in a High Subsonic Mach Number Turbulent Jet , 2005 .

[15]  R. Adrian Stochastic Estimation of the Structure of Turbulent Fields , 1996 .

[16]  William K. George,et al.  The reduction of spatial aliasing by long hot-wire anemometer probes , 1997 .

[17]  Charles E. Tinney,et al.  POD based experimental flow control on a NACA-4412 airfoil (invited) , 2004 .

[18]  Julius S. Bendat,et al.  Engineering Applications of Correlation and Spectral Analysis , 1980 .

[19]  Joël Delville,et al.  La décomposition orthogonale aux valeurs propres et l'analyse de l'organisation tridimensionnelle des écoulements turbulents cisaillés libres , 1995 .

[20]  Ronald Adrian,et al.  Higher‐order estimates of conditional eddies in isotropic turbulence , 1980 .

[21]  Joel Delville,et al.  Pressure Velocity Coupling in a Subsonic Round Jet , 1999 .

[22]  Fabienne Ricaud,et al.  Etude de l'identification des sources acoustiques à partir du couplage de la pression en champ proche et de l'organisation instantanée de la zone de mélange de jet , 2003 .

[23]  J. Lumley,et al.  A First Course in Turbulence , 1972 .

[24]  Joel Delville,et al.  Pressure velocity coupling in a subsonic round jet , 2000 .

[25]  Ronald Adrian,et al.  Conditional eddies in isotropic turbulence , 1979 .

[26]  Jean-Paul Bonnet Eddy structure identification , 1996 .

[27]  A. Hussain,et al.  On the coherent structure of the axisymmetric mixing layer: a flow-visualization study , 1981, Journal of Fluid Mechanics.

[28]  Y. Gervais,et al.  Coherent Structures in Subsonic Jets: A Quasi-Irrotational Source Mechanism? , 2006 .

[29]  N. W. M. Ko,et al.  The near field within the potential cone of subsonic cold jets , 1971, Journal of Fluid Mechanics.

[30]  Mark N. Glauser,et al.  APPLICATIONS OF STOCHASTIC ESTIMATION IN THE AXISYMMETRIC SUDDEN EXPANSION , 1998 .

[31]  Mark N. Glauser,et al.  Stochastic estimation and proper orthogonal decomposition: Complementary techniques for identifying structure , 1994 .

[32]  A. Naguib,et al.  Stochastic estimation and flow sources associated with surface pressure events in a turbulent boundary layer , 2001 .