Please use this identifier to cite or link to this item: http://scholarbank.nus.edu.sg/handle/10635/73924
Title: The analysis of cyclogyro using Unsteady Vortex Lattice Method
Authors: Yu, H. 
Beng, T.W.
Bin, L.K. 
Keywords: Cyclogyro
Cycloidal propeller
MAV
Unsteady Vortex Lattice method
Issue Date: 2006
Source: Yu, H.,Beng, T.W.,Bin, L.K. (2006). The analysis of cyclogyro using Unsteady Vortex Lattice Method. ICAS-Secretariat - 25th Congress of the International Council of the Aeronautical Sciences 2006 2 : 930-935. ScholarBank@NUS Repository.
Abstract: The investigation on analysis of a cyclogyro using Unsteady Vortex Lattice Method (UVLM) is presented in this paper. There exists many simplified method for cyclogyro design analysis, but they are quite crude and do not fully deal with problems with complex configurations and motion patterns. By solving N-S equations using the CFD algorithms can solve the problem but the cost is too high. The UVLM is a good choice in this case since it can solve very complex configuration with complicated wing motion pattern. It only needs to generate grids on wing surfaces and wake. So UVLM is selected for the design simulation of cyclogyro in this paper. The comparison was made between the UVLM and the experiment data. The comparison indicates that UVLM can provide good results for cycloidal propellers and can be applied in the design analysis of cyclogyroes.
Source Title: ICAS-Secretariat - 25th Congress of the International Council of the Aeronautical Sciences 2006
URI: http://scholarbank.nus.edu.sg/handle/10635/73924
ISBN: 9781604232271
Appears in Collections:Staff Publications

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