TY - GEN
T1 - Low-order models of the fluctuating wall pressure in an incompressible turbulent impinging jet
AU - Hall, Joseph W.
AU - Ausseur, Julie
AU - Pinier, Jeremy T.
AU - Glauser, Mark N.
PY - 2006
Y1 - 2006
N2 - The fluctuating wall pressure field measured simultaneously at 137 points in an impinging jet with ReD=23,000 and a nozzle-to-plate spacing of two diameters. A previous time averaged azimuthal decomposition1 indicated that the fluctuating pressure field could be accurately described using few azimuthal modes, indicating this flow is an excellent candidate for a Low-Order Dynamical Systems (LODS) model. The present model was developed using a method similar as Ricaud,2 whereby a general cubic order system of equations is fit to the experimentally determined Fourier coefficients. A LODS model developed using only azimuthal modes 0, 1 and 2 was able to reasonably accurately capture the behaviour of the fluctuating pressure field at r/D = 1.5. Downstream at r/D = 2.0, where the pressure field is more three-dimensional, the addition of azimuthal mode 3 is required to produce a stable system of equations, that again, reasonably captures the dynamics of the fluctuating pressure field. The success of this technique here, suggests that it may prove useful in high speed flow control applications where some degree of predictive ability is required.
AB - The fluctuating wall pressure field measured simultaneously at 137 points in an impinging jet with ReD=23,000 and a nozzle-to-plate spacing of two diameters. A previous time averaged azimuthal decomposition1 indicated that the fluctuating pressure field could be accurately described using few azimuthal modes, indicating this flow is an excellent candidate for a Low-Order Dynamical Systems (LODS) model. The present model was developed using a method similar as Ricaud,2 whereby a general cubic order system of equations is fit to the experimentally determined Fourier coefficients. A LODS model developed using only azimuthal modes 0, 1 and 2 was able to reasonably accurately capture the behaviour of the fluctuating pressure field at r/D = 1.5. Downstream at r/D = 2.0, where the pressure field is more three-dimensional, the addition of azimuthal mode 3 is required to produce a stable system of equations, that again, reasonably captures the dynamics of the fluctuating pressure field. The success of this technique here, suggests that it may prove useful in high speed flow control applications where some degree of predictive ability is required.
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U2 - 10.2514/6.2006-3699
DO - 10.2514/6.2006-3699
M3 - Conference contribution
AN - SCOPUS:33845251823
SN - 1563478137
SN - 9781563478130
T3 - Collection of Technical Papers - 3rd AIAA Flow Control Conference
SP - 1759
EP - 1770
BT - Collection of Technical Papers - 3rd AIAA Flow Control Conference
PB - American Institute of Aeronautics and Astronautics Inc.
T2 - 3rd AIAA Flow Control Conference
Y2 - 5 June 2006 through 8 June 2006
ER -