JEB -- Sunada et al. 205 (17): 2737 Figure IG2

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Fig. 2. Experimental apparatus used to measure the fluid-dynamic forces of a wing in forward motion (constant-velocity translation and accelerating translation). X, Y, Z, earth-fixed coorinate system; x, y, z, wing-fixed coordinate system; L_X, L_Y, L_Z, dimensions of the tank; ${alpha}$ , angle of attack.