Host: The Japan Society of Mechanical Engineers
Name : [in Japanese]
Date : September 11, 2022 - September 14, 2022
The effect of feathering motion during flapping flight on aerodynamic characteristics is numerically studied for an enlarged model of a mosquito wing by using OpenFOAM together with immersed boundary method. It is shown that aerodynamic performance is improved because the separated region is reduced by feathering motion.