2008Kongqi donglixue xuebaoRequires access

Flow field characteristics of wing tips vortex and its control

Zheng Xin-jun

Open publisher page 1 citations

Abstract

It is very dangerous for small airplane encountering the wake vortices flow of large transport aircraft.Specific vortex control device is need to decrease the vortices strengthen.The flow field of the wing tip vortex,which shed from a rectangular wing,is surveyed by a seven holes probe in a low speed wind tunnel.The features of wingtip vortex various with angle of attack of the wing and its development to two chord lengths down-stream from trailing edge are given.Some vortex diffusers are deployed at wing tip to control the vortex.The wing tips vortex is separated into two weaker vortices.The flow field measurement results show that the strength of wingtip-vortex can be obviously decreased with control of vortex diffusers.

About this research paper

What this paper is about

It is very dangerous for small airplane encountering the wake vortices flow of large transport aircraft.Specific vortex control device is need to decrease the vortices strengthen.The flow field of the wing tip vortex,which shed from a rectangular wing,is surveyed by a seven holes probe in a low speed wind tunnel.The features of wingtip vortex various with angle of attack of the wing and its development to two chord lengths down-stream from trailing edge are given.Some vortex diffusers are deployed at wing tip to control the vortex.The wing tips vortex is separated into two weaker vortices.The flow field measurement results show that the strength of wingtip-vortex can be obviously decreased with control of vortex diffusers.

Why it matters

OpenAlex reports 1 citations for this work. Citation counts describe recorded attention and do not establish research quality.

Key contribution

A contribution statement is not available in the OpenAlex record.

Method / approach

Method details are not available in the OpenAlex metadata.

Main findings

Findings are not separately available in the OpenAlex metadata.

Limitations

Limitations are not available in the OpenAlex metadata.

Applications

Application details are not available in the OpenAlex metadata.

Available abstract

It is very dangerous for small airplane encountering the wake vortices flow of large transport aircraft.Specific vortex control device is need to decrease the vortices strengthen.The flow field of the wing tip vortex,which shed from a rectangular wing,is surveyed by a seven holes probe in a low speed wind tunnel.The features of wingtip vortex various with angle of attack of the wing and its development to two chord lengths down-stream from trailing edge are given.Some vortex diffusers are deployed at wing tip to control the vortex.The wing tips vortex is separated into two weaker vortices.The flow field measurement results show that the strength of wingtip-vortex can be obviously decreased with control of vortex diffusers.

Key concepts: Wingtip vortices, Vortex, Horseshoe vortex, Wing, Starting vortex, Vortex shedding, Vortex generator, Wind tunnel

Related papers

Back to paper searchBrowse research topicsOriginal source
Flow field characteristics of wing tips vortex and its control — Research Paper | ScholarLens