Dynamic Mode Decomposition Analysis of Flow Separation in a Diffuser to Inform Flow Control Strategies

2019 ◽  
Vol 142 (2) ◽  
Author(s):  
Jinchun Wang ◽  
Guoping Huang ◽  
Weiyu Lu ◽  
Pierre E. Sullivan

Abstract In this work, a large eddy simulation (LES) of a typical subsonic diffuser provides data used to analyze coherent structure in a separated flow with dynamic mode decomposition (DMD). From this, a low–dimensional approximation, which retains the main dynamic characteristics of the original flow fields, is obtained. In particular, specific dynamic structures associated with a unique frequency are isolated. The spatial structures of the real and imaginary parts of the DMD mode are similar but with a phase difference. The contribution of the conjugate modes to the evolution of the DMD modes over time is discussed. The dominant frequency is found to be related to the wake mode. The scale of wake will saturate, and the shear layer will become weaker and merges into the wake structure as it develops downstream. This allows direction for effective flow control strategies using this information.

2020 ◽  
Vol 105 (3) ◽  
pp. 699-713 ◽  
Author(s):  
Hadrien Calmet ◽  
Daniel Pastrana ◽  
Oriol Lehmkuhl ◽  
Takahisa Yamamoto ◽  
Yoshiki Kobayashi ◽  
...  

2019 ◽  
Vol 11 (6) ◽  
pp. 063307
Author(s):  
Mohammad Hossein Naderi ◽  
Mojtaba Tahani ◽  
Vahid Esfahanian

2017 ◽  
Vol 27 (11) ◽  
pp. 2528-2543 ◽  
Author(s):  
Liang Wang ◽  
Liying Li ◽  
Song Fu

Purpose The purpose of this paper is to numerically investigate the mildly separated flow phenomena on a near-stall NACA0015 airfoil, by using Detached-Eddy Simulation (DES) type methods. It includes a comparison of different choices of underlying Reynolds-averaged Navier–Stokes model as well as subgrid-scale stress model in Large-Eddy simulation mode. Design/methodology/approach The unsteady flow phenomena are simulated by using delayed DES (DDES) and improved DDES (IDDES) methods, with an in-house computational fluid dynamics solver. Characteristic frequencies in different flow regions are extracted using fast Fourier transform. Dynamic mode decomposition (DMD) method is applied to uncover the critical dynamic modes. Findings Among all the DES type methods investigated in this paper, only the Spalart–Allmaras-based IDDES captures the separation point as measured in the experiments. The classical vortex-shedding and the shear-layer flapping modes for airfoil flows with shallow separation are also found from the IDDES results by using DMD. Originality/value The value of this paper lies in the assessment of five different DES-type models through the detailed investigation of the Reynolds stresses as well as the separation and reattachment.


2020 ◽  
Vol 94 ◽  
pp. 102901 ◽  
Author(s):  
P. Neumann ◽  
V.B.C. de Almeida ◽  
V. Motta ◽  
L. Malzacher ◽  
D. Peitsch ◽  
...  

2012 ◽  
Vol 24 (6) ◽  
pp. 066101 ◽  
Author(s):  
L. Massa ◽  
R. Kumar ◽  
P. Ravindran

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