Performance assessment of transition models for three-dimensional flow over NACA4412 wings at low Reynolds numbers

İ Karasu, M Özden, MS Genç - Journal of Fluids …, 2018 - asmedigitalcollection.asme.org
The performance of the transition models on three-dimensional (3D) flow of wings with
aspect ratios (AR) of 1 and 3 at low Reynolds number was assessed in this study. For …

On the controlled evolution for wingtip vortices of a flapping wing model at bird scale

S Qin, Z Weng, Z Li, Y Xiang, H Liu - Aerospace Science and Technology, 2021 - Elsevier
The reduction of wingtip vortices is a critical and challenging task for aircraft wing-design.
Inspired by the wingtip morphology of soaring birds, Whitcomb created winglets to reduce …

[PDF][PDF] Wing in ground effect craft: a review of the state of current stability knowledge

MAU Amir, A Maimun, S Mat, MR Saad… - … Conference on Ocean …, 2016 - isomase.org
Wing in ground effect craft are becoming promising transportation over the last decade. This
paper objectively reviews the current state of knowledge of stability wing in ground effect …

An experimental investigation of wing-tip vortex decay in turbulence

HC Ghimire, SCC Bailey - Physics of Fluids, 2017 - pubs.aip.org
Particle image velocimetry measurements were conducted for a wing-tip vortex decaying in
free-stream turbulence. The vortex exhibited stochastic collapse with free-stream turbulence …

[HTML][HTML] Study on decay characteristics of vertical four-vortex system for increasing airport capacity

J Cho, BJ Lee, T Misaka, K Yee - Aerospace Science and Technology, 2020 - Elsevier
The wake vortices of an aircraft descend by self-induction that enables a pilot to identify
approximate wake location based on the preceding aircraft path. A pilot taking off an aircraft …

Effect of a directionally porous wing tip on tip vortex

M Aldheeb, W Asrar, A Omar, A Altaf… - Journal of Applied Fluid …, 2020 - jafmonline.net
This paper presents an experimental study of the effect of a directionally porous wing tip on
the tip vortex using particle image velocimetry (PIV) on a half wing model with NACA 653218 …

Experimental study of wingtip vortices behind the finite-span wing

RP Stepanov, AN Kusyumov, SA Mikhailov… - Trudy MAI, 2019 - trudymai.ru
The article presents the results of experimental study of wingtip vortices behind a
rectangular wing of a finite-span in the near field (at a distance of 0.5 to 4.2 wing chords …

[HTML][HTML] Экспериментальное исследование концевых вихрей за крылом конечного размаха

РП Степанов, АН Кусюмов, СА Михайлов… - Труды …, 2019 - cyberleninka.ru
Представлены результаты экспериментального исследования концевых вихрей за
прямоугольным крылом конечного размаха в ближнем поле (на расстоянии от 0, 5 до 4 …

Near field of a vortex generated by chevron-tipped flat plates

A Goyal, J Nedić - AIAA Journal, 2021 - arc.aiaa.org
Flat plates with chevron tips of variable depths (2 h) were designed and their effect on the tip
vortex was studied at downstream distances of x= 0.5 c to 3 c at a Reynolds number of …

Numerical simulation and validation of influence of end clearance in half vane diffuser on hydraulic performance for centrifugal pump

W Jiang, D Chen, Y Qin, Y Wang - Transactions of the Chinese …, 2017 - ingentaconnect.com
Centrifugal pumps are widely used in general machines and the demand of the efficiency
and the stable operation can be more and more high. All kinds of clearance appear easily in …