Horn-Schunck optical flow applied to deformation measurement of a birdlike airfoil

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Current deformation measurement techniques suffer from limited spatial resolution. In this work, a highly accurate and high-resolution Horn-Schunck optical flow method is developed and then applied to measuring the static deformation of a birdlike flexible airfoil at a series of angles of attack at Reynolds number 100,000 in a low speed, low noise wind tunnel. To allow relatively large displacements, a nonlinear Horn-Schunck model and a coarse-to-fine warping process are adopted. To preserve optical flow discontinuities, a nonquadratic penalization function, a multi-cue driven bilateral filtering and a principle component analysis of local image patterns are used. First, the accuracy and convergence of this Horn-Schunck technique are verified on a benchmark. Then, the maximum displacement that can be reliably calculated by this technique is studied on synthetic images. Both studies are compared with the performance of a Lucas-Kanade optical flow method. Finally, the Horn-Schunck technique is used to estimate the 3-D deformation of the birdlike airfoil through a stereoscopic camera setup. The results are compared with those computed by Lucas-Kanade optical flow, image correlation and numerical simulation.




Gong, X., & Bansmer, S. (2015). Horn-Schunck optical flow applied to deformation measurement of a birdlike airfoil. Chinese Journal of Aeronautics, 28(5), 1305–1315. https://doi.org/10.1016/j.cja.2015.07.005

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