Measurements of aircraft wake vortices in ground proximity within an atmospheric boundary layer wind tunnel
Loading...
Date published
Free to read from
Authors
Fonti, Elio
Supervisor/s
Journal Title
Journal ISSN
Volume Title
Publisher
Department
Course name
ISSN
Format
Citation
Abstract
The vortex wake characteristics of aircraft during landing and take-off are of interest in connection with both the safety of following aircraft penetrating the vortex and the dispersion of engine exhaust plumes. A series of measurements were carried out in an Atmospheric Boundary Layer Wind Tunnel (ABLWT) to identify and characterise both the mean and turbulent flow field of a pair of wake vortices in ground proximity. Cont/d.
Description
Software Description
Software Language
Github
Keywords
DOI
Rights
© Cranfield University 2010. All rights reserved. No part of this publication may be
reproduced without the written permission of the copyright owner.