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Dynamical modeling of the flow over flapping wing by applying proper orthogonal decomposition and system identification
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index.pdf
Date
2011
Author
Durmaz, Oğuz
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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 state space dynamical model to the trajectories of the time coefficients using subspace system identification (N4SID). The procedure is applied using MATLAB for the data obtained from NACA 0012, SD 7003, elliptic airfoil and flat plate, and the results show that the dynamical model obtained can represent the flow dynamics with acceptable accuracy.
Subject Keywords
Vehicles, Remotely piloted.
,
Airplanes
URI
http://etd.lib.metu.edu.tr/upload/12613549/index.pdf
https://hdl.handle.net/11511/20878
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Graduate School of Natural and Applied Sciences, Thesis
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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
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Dynamical modelling of the flow over a flapping wing using proper orthogonal decomposition and system identification techniques
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O. Durmaz, “Dynamical modeling of the flow over flapping wing by applying proper orthogonal decomposition and system identification,” M.S. - Master of Science, Middle East Technical University, 2011.
