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Dynamical Modeling of the Unsteady Flow over a Flapping Wing by applying Proper Orthogonal Decomposition and System Identification to Particle Image Velocimetry Data
Date
2011-12-15
Author
Durmaz, Oguz
Karaca, H. Deniz
Ozen, G. Deniz
KASNAKOĞLU, Coşku
Kurtuluş, Dilek Funda
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Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International License
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In this work a novel approach for the dynamical modeling of the unsteady flow over a pitching airfoil is considered. The technique is based on collecting instantaneous velocity field data of the flow using particle image velocimetry (PIV), applying image processing to these snapshots to locate the airfoil, filling the airfoil and its surface with proper velocity data, applying proper orthogonal decomposition (POD) to these post-processed images to compute the POD modes and time coefficients, and finally fitting a discrete time state space dynamical model to the trajectories of the time coefficients using subspace system identification (N4SID). The procedure is implemented using MATLAB for the data obtained from a NACA0012 airfoil, and the results show that the dynamical model obtained can represent the flow dynamics with acceptable accuracy.
Subject Keywords
Reduction
,
Transient
URI
https://hdl.handle.net/11511/55054
Conference Name
50th IEEE Conference of Decision and Control (CDC)/European Control Conference (ECC)
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Department of Aerospace Engineering, Conference / Seminar
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Dynamical modeling of the flow over flapping wing by applying proper orthogonal decomposition and system identification
Durmaz, Oğuz; Kurtuluş, Dilek Funda; Kasnakoğlu, Coşku; Department of Aerospace Engineering (2011)
In this study the dynamical modeling of the unsteady flow over a flapping wing is considered. The technique is based on collecting instantaneous velocity field data of the flow using Particle Image Velocimetry (PIV), applying image processing to these snapshots to locate the airfoil, filling the airfoil and its surface with proper velocity data, applying Proper Orthogonal Decomposition (POD) to these post-processed images to compute the POD modes and time coefficients, and finally fitting a discrete time st...
Dynamical modelling of the flow over a flapping wing using proper orthogonal decomposition and system identification techniques
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O. Durmaz, H. D. Karaca, G. D. Ozen, C. KASNAKOĞLU, and D. F. Kurtuluş, “Dynamical Modeling of the Unsteady Flow over a Flapping Wing by applying Proper Orthogonal Decomposition and System Identification to Particle Image Velocimetry Data,” presented at the 50th IEEE Conference of Decision and Control (CDC)/European Control Conference (ECC), Orlando, FL, 2011, Accessed: 00, 2020. [Online]. Available: https://hdl.handle.net/11511/55054.