2005
DOI: 10.1063/1.1990206
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Decomposition of the spatially filtered and ensemble averaged kinetic energy, the associated fluxes and scaling trends in a rotor wake

Abstract: Particle image velocimetry data obtained in the rotor wake of a turbomachine are used for examining elements of the ensemble averaged and spatially filtered kinetic energy. These two distinct averaging processes decompose the kinetic energy into four parts, consisting of the mean-flow resolved, mean-flow subgrid, fluctuating resolved, and fluctuating subgrid parts. Their evolution equations include energy flux terms among these parts. The results elucidate the fundamental difference between the filtered turbul… Show more

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Cited by 22 publications
(7 citation statements)
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“…Rivera et al (2003); Chen et al (2003); Rivera et al (2014)), to experiments of turbulent jets Liu et al (1994) and flows through a grid Meneveau (1994), through a duct Tao et al (2002), in a water channel Bai et al (2013), and in turbomachinery (e.g. Chow et al (2005); Akbari and Montazerin (2013)). Moreover, the framework has been extended to rotating stratified flows Aluie and Kurien (2011), magnetohydrodynamics Aluie (2017b), and compressible turbulence (e.g.…”
Section: The Coarse-graining Methodsmentioning
confidence: 99%
“…Rivera et al (2003); Chen et al (2003); Rivera et al (2014)), to experiments of turbulent jets Liu et al (1994) and flows through a grid Meneveau (1994), through a duct Tao et al (2002), in a water channel Bai et al (2013), and in turbomachinery (e.g. Chow et al (2005); Akbari and Montazerin (2013)). Moreover, the framework has been extended to rotating stratified flows Aluie and Kurien (2011), magnetohydrodynamics Aluie (2017b), and compressible turbulence (e.g.…”
Section: The Coarse-graining Methodsmentioning
confidence: 99%
“…In the inertial subrange of homogenous, isotropic turbulence, SGS is almost equal to (Pope 2000). The in-plane contribution to the SGS energy flux, SGS 2D (⌬), is (Liu et al 1999;Chow et al 2005;Chen et al 2005) 2D SGS ͑⌬͒ ϭ Ϫ͑ 11 S 11 ϩ 33 S 33 ͒ Ϫ 2 13 S 13 , ͑7͒…”
Section: Sgsmentioning
confidence: 99%
“…This applies not only to the design of new turbomachinery, but also during the refurbishment process of existing aeroengines. It requires detailed knowledge of the aerodynamics of multistage turbomachinery, including unsteady boundary layer development and transition [2,3], wake development [4,5], and interaction of the wakes with downstream blades [6,7].…”
Section: Resulting Aerodynamic Losses Of Combinations Of Localized Romentioning
confidence: 99%