The shape and function of insect wings tremendously vary between insect species. This review is engaged in how wing design determines the aerodynamic mechanisms with which …
Z Wei, TH New, YD Cui - Ocean Engineering, 2015 - Elsevier
Hydrodynamic characteristics of hydrofoils with leading-edge tubercles were experimentally investigated in a water tunnel at a Reynolds number of Re= 1.4× 10 4. Particle image …
Z Guo, W Xia, Z Qian - Ocean Engineering, 2022 - Elsevier
The effects of wavy leading edge on noise of an axial flow waterjet pump are investigated by using numerical simulation method. Based on bionics, five wavy leading edges with different …
The phenomenon of insect flight has been of scientific interest for many years and is more recently inspiring modern engineering devices such as Micro Aerial Vehicles (MAVs). Insect …
N Chitsaz, K Siddiqui, R Marian, J Chahl - Experimental Thermal and Fluid …, 2021 - Elsevier
In this paper, an experimental study was performed to examine the flow characteristics of fabricated micro corrugated wings by fully mimicking the real 3D Odonata wing. For this …
T Engels, HN Wehmann… - Journal of the Royal …, 2020 - royalsocietypublishing.org
The aerial performance of flying insects ultimately depends on how flapping wings interact with the surrounding air. It has previously been suggested that the wing's three-dimensional …
H Yu, H Hu, WL Chen, Y Lu, D Gao - Physics of Fluids, 2024 - pubs.aip.org
Flow modulation mechanism in a cylinder with corrugated surfaces is investigated by wind tunnel experiments at Reynolds number R e= 25 600. Experimental results include surface …
Flow past a backward facing ramp (BFR) with rectangular vane-type vortex generators (VGs) located upstream has been studied numerically using OpenFOAM based steady-state RANS …
WH Ho, TH New - … of the Institution of Mechanical Engineers …, 2017 - journals.sagepub.com
An unsteady, two-dimensional numerical study was conducted to investigate the aerodynamic and flow characteristics of two bio-inspired corrugated airfoils at Re= 14,000 …