Mathematical modelling for compliance-assisted artificial muscle based ornithopter

R Pachamuthu, AT Biju, S Madupu - Aircraft Engineering and …, 2024 - emerald.com
Purpose This study aims to discuss the mathematical modelling of a compliance-assisted
flapping mechanism and morphable structures for an UAV. Design/methodology/approach A …

[PDF][PDF] Aerodynamic Analysis and Design Optimization of a Novel Flapping Wing Micro Air Vehicle in Hovering Flight

Y Zhang, Z Wang, H Zheng - Journal of Applied Fluid Mechanics, 2023 - jafmonline.net
Inspired by the challenging and nimble flight dynamics of flying insects and birds, this
research investigates bionic propulsion technology to develop an improved flapping wing …

Effect of chord-wise flexibility in the lift generation of flapping MAV with membrane wing

S Syam Narayanan, R Asad Ahmed - Aircraft Engineering and …, 2022 - emerald.com
Purpose The purpose of this study is to experimentally analyse the effect of flexible and
stiffened membrane wings in the lift generation of flapping micro air vehicle (MAV) …

Analysis of the sound field characteristics of a muffler at different flow conditions

JW Lin, HL Liu, L Dong, RZ Zhou… - Journal of Applied Fluid …, 2022 - jafmonline.net
To reduce the noise in a pump piping system and increase the usage time of equipment, a
new type of porous muffler is proposed in this paper. A water guide cone is incorporated into …

Aerodynamic Performance of Lambda Wing-UCAV at Different Back-sweep Angles

S Syam Narayanan, Y Gangurde… - Journal of Applied Fluid …, 2024 - jafmonline.net
Unmanned Combat Aerial Vehicles (UCAVs) are designed to be lightweight and compact,
which can impact their overall lift and aerodynamic capabilities. This study focuses on …