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- W161688280 abstract "An extension of nonintrusive approach based on an integral form of the momentum equation is proposed to evaluate instantaneous loads of a NACA0012 airfoil in flapping motion at Re = 1000 (The Reynolds number is based on the chord length and the velocity at 2/3 of the wingspan) in the case of the three-dimensional PIV measurements. Two major difficulties of this approach in 3D are the quality of the time-resolved volumic velocity fields and the estimation of the pressure field on the surface of the control volume. This last step needs a good spatial and temporal resolution of the velocity fields. Experimental data are issued from a scanning tomography PIV technique for a flapping wing in revolving motion. The volumes of particles are reconstructed using the 100 images of the acquisition, and the three-dimensional velocity fields around the airfoil are evaluated with an adaptive 3D cross-correlation. Phase-averaged velocity fields are estimated from the 25 velocity fields and are used by an iterative algorithm based on Navier-Stokes equations to deduce the pressure on the surfaces of the control volume. A special interest on the accuracy of the method is achieved. The results of the pressure fields and the load evaluation demonstrate the feasibility of the method and will provide new sets of data to better understand the effects of the 3D vortex structures on the wing lift in flapping motion." @default.
- W161688280 created "2016-06-24" @default.
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- W161688280 date "2013-07-01" @default.
- W161688280 modified "2023-09-24" @default.
- W161688280 title "Loads and pressure evaluation of the flow around a flapping wing" @default.
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