J0205-1-5 Study on the Aerodynamic Forces Generated by a Flapping Membrane Wing

Abstract

In this study, we have developed synchronized continuous stroboscopic photography with high resolution for observation of the moving membrane wing. We also have developed a calculation program for the analysis of the results obtained using DLT (Direct Linear Transformation) method for motion analysis of 3-demensions. We have successfully applied measurement results obtained by the method described above to CFD (Computational Fluid Dynamics) program.