Volume grid deformation code for numerical simulation of a flapping foil
As a nature-inspired technology,flapping foils have attracted much attention due to that they are capable to produce thrust with high efficiency.For this reason,flapping foils have been used as the thrust engine of micro-air vehicles.In design stage of the micro-air vehicles,computationalfluid dynamics (CFD)is typically employed for the numerical simulation of the flapping foils and should consider large deformation of moving boundaries.Therefore,it becomes a challenging problem in the CFD analysis to develop robust,efficient grid deformation algorithms for the large deformation.
Jin-Hwan Ko Jee Woong Kim Doyoung Buyn Soo Hyung Park
Dept.of Aerospace Information Eng.,Konkuk University,Seoul,Korea
国际会议
南京
英文
90-91
2008-10-01(万方平台首次上网日期,不代表论文的发表时间)