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Triple decomposition is a powerful analytical method for a deep understanding of the flow structure by extracting the mean value, organized coherent motion, and stochastic part from a fluctuating quantity. Here, we perform the triple decomposition of the spatial two-dimensional data, especially pressure-sensitive paint (PSP) data, since the PSP method is widely used to measure the pressure distribution on a surface in wind tunnel testing. However, the PSP data measuring near atmospheric pressure contain significant noise, and this makes it difficult to conduct the decomposition. To construct phase-averaged data representing an organized coherent motion, we propose a relatively simple method based on a multi-dimensional scaling plot of the cosine similarity between each PSP datum. Then, the stochastic part is extracted by selecting phase-averaged data with an appropriate phase angle based on the similarity between the measurement and phase-averaged data, and the PSP data are successfully decomposed. Moreover, we consider sparse optimal sensor positions, in which the data are effectively represented, based on the stochastic part as a data-driven approach. The optimal sensor positions are determined as a combinatorial optimization problem and estimated using Fujitsu computing as a service digital annealer. We reconstruct the pressure distribution from the pressure data at the optimal sensor positions using the mean value, organized coherent motion, and stochastic part obtained from the triple decomposition. The root mean square error between the pressure measured by a pressure transducer and the reconstructed pressure obtained by the proposed method is small, even when the number of modes and sensor points is small. The application of PSP measurement is expected to expand further, and the framework for calculating triple decomposition and sparse representation based on the decomposition will be useful for detailed flow analysis.
Triple decomposition is a powerful analytical method for a deep understanding of the flow structure by extracting the mean value, organized coherent motion, and stochastic part from a fluctuating quantity. Here, we perform the triple decomposition of the spatial two-dimensional data, especially pressure-sensitive paint (PSP) data, since the PSP method is widely used to measure the pressure distribution on a surface in wind tunnel testing. However, the PSP data measuring near atmospheric pressure contain significant noise, and this makes it difficult to conduct the decomposition. To construct phase-averaged data representing an organized coherent motion, we propose a relatively simple method based on a multi-dimensional scaling plot of the cosine similarity between each PSP datum. Then, the stochastic part is extracted by selecting phase-averaged data with an appropriate phase angle based on the similarity between the measurement and phase-averaged data, and the PSP data are successfully decomposed. Moreover, we consider sparse optimal sensor positions, in which the data are effectively represented, based on the stochastic part as a data-driven approach. The optimal sensor positions are determined as a combinatorial optimization problem and estimated using Fujitsu computing as a service digital annealer. We reconstruct the pressure distribution from the pressure data at the optimal sensor positions using the mean value, organized coherent motion, and stochastic part obtained from the triple decomposition. The root mean square error between the pressure measured by a pressure transducer and the reconstructed pressure obtained by the proposed method is small, even when the number of modes and sensor points is small. The application of PSP measurement is expected to expand further, and the framework for calculating triple decomposition and sparse representation based on the decomposition will be useful for detailed flow analysis.
Flow around the D-shaped cylinder is one of the basic models in aerospace, civil, and marine engineering applications. This paper reports an experimental work on the optimization control of the D-shaped cylinder flow using genetic algorithm (GA) and Coanda pulsation jets. Experiments are conducted in a wind tunnel at a Reynolds number Re = 2.0 × 104, based on free stream velocity U∞ and the cylinder height H. The Coanda pulsation jets are realized by issuing pulsation jets over the surface of a one-quarter cylinder (radius r = 0.2H), which is attached on the base and near the trailing edge of the D-shaped cylinder. Control parameters of the Coanda pulsation jets include momentum coefficient (Cμ), nondimensional pulsation frequency (fj*), duty cycle (DC), and phase shift (Δϕ) between the lower and upper jets. GA is adopted to seek optimal working parameters of the Coanda pulsation jets for the maximum recovery of base pressure (indicating drag reduction). The near wake flow of the D-shaped cylinder under optimal control is measured using particle image velocimetry, and then, thoroughly examined using proper orthogonal decomposition (POD), to investigate underlying mechanisms of drag reduction. Two sets of optimal control parameters differing in fj* and Δϕ are identified by the GA-based optimization control, corresponding to the maximum base pressure recovery of 40.7%–43.3%. Significant modifications in the near wake flows are observed in the presence of the optimal control, based on instantaneous, time-mean and phase-averaged flow structures, Reynolds stresses, as well as the POD analyses. It is found that the Coanda pulsation jets working at the different sets of optimal parameters render distinct perturbations to the near wake flows, weakening the large-scale Karman vortices while energizing the small-scale structures.
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