Numerical and experimental studies of a morphing airfoil with trailing edge high-frequency flapping
Author:
Affiliation:
1. College of Aerospace Science and Engineering, National University of Defense Technology 1 , Changsha, Hunan 410073, China
2. China Aerodynamics Research and Development Center 2 , Mianyang, Sichuan 621000, China
Abstract
Funder
National Natural Science Foundation of China
Publisher
AIP Publishing
Subject
Condensed Matter Physics,Fluid Flow and Transfer Processes,Mechanics of Materials,Computational Mechanics,Mechanical Engineering
Link
https://pubs.aip.org/aip/pof/article-pdf/doi/10.1063/5.0174349/18253524/121904_1_5.0174349.pdf
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3. Numerical investigation of an insect-scale flexible wing with a small amplitude flapping kinematics;Phys. Fluids,2022
4. Novel morphing wing actuator control-based particle swarm optimisation;Aeronaut. J.,2019
5. Numerical simulation investigation on the suction stroke and blowing stroke of synthetic jet circulation control;Acta Mech. Sin.,2023
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