A vortex approach for unsteady insect flight analysis in 2D
Author:
Affiliation:
1. Mechanical and Aerospace Engineering Department, Rutgers University, Piscataway, NJ, USA.
Publisher
River Publishers
Subject
Mechanical Engineering,Mechanics of Materials,Modeling and Simulation
Link
https://www.tandfonline.com/doi/pdf/10.1080/17797179.2016.1199236
Reference16 articles.
1. Non-linear unsteady aerodynamic model for insect-like flapping wings in the hover. Part 1: Methodology and analysis
2. Non-linear unsteady aerodynamic model for insect-like flapping wings in the hover. Part 2: Implementation and validation
Cited by 3 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Comparative study between a discrete vortex method and an immersed boundary–lattice Boltzmann method in 2D flapping flight analysis;International Journal of Modern Physics C;2020-10-21
2. The 2D lumped wake vortex method applied to unsteady flapping;International Journal of Intelligent Unmanned Systems;2020-06-15
3. A simple vortex approach to complex two-wing unsteady flapping problems in 2D applied to insect flight study;European Journal of Computational Mechanics;2018-12-10
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