Flapping propulsion of low aspect-ratio wing with morphing trailing edge: Lattice Boltzmann simulation
Authors:
- Tianlong LinTLTianlong Lin
- Wei XiaWXWei Xia
- Rosario PecoraRosario Pecora
- Kun WangKWKun Wang
- Liang JiLJLiang Ji
- Shuling HuSHShuling Hu
- 5 August 2025
- journal article
- Published by Elsevier in Aerospace Science and Technology
- Vol. 167
Abstract
No abstract availableFunding Information
- Project 211 (B18040)
- Xi'an Jiaotong University
- National Natural Science Foundation of China (12172275)
- National Natural Science Foundation of China (12090030)
This publication has 49 references indexed in Scilit:
- Numerical analysis of the wing–wake interaction of tandem flapping wings in forward flightAerospace Science and Technology, 2022
- Effects of wing kinematics, corrugation, and clap-and-fling on aerodynamic efficiency of a hovering insect-inspired flapping-wing micro air vehicleAerospace Science and Technology, 2021
- Interaction of the wakes of two flapping wings on control forces and momentAerospace Science and Technology, 2021
- Design, aerodynamic analysis and test flight of a bat-inspired tailless flapping wing unmanned aerial vehicleAerospace Science and Technology, 2021
- The modeling and numerical solution for flapping wing hovering wingbeat dynamicsAerospace Science and Technology, 2021
- Palabos: Parallel Lattice Boltzmann SolverComputers & Mathematics with Applications, 2021
- Aero-servo-elastic design of a morphing wing trailing edge system for enhanced cruise performanceAerospace Science and Technology, 2019
- Numerical investigation of the effects of different parameters on the thrust performance of three dimensional flapping wingsAerospace Science and Technology, 2019
- Symmetrical and non-symmetrical 3D wing deformation of flapping micro aerial vehiclesAerospace Science and Technology, 2016
- Effect of internal mass in the simulation of a moving body by the immersed boundary methodComputers & Fluids, 2011