Measurements of aircraft wake vortices in ground proximity within an atmospheric boundary layer wind tunnel

Simple item page
dc.contributor.advisorGarry, Kevin P.
dc.contributor.advisorLawson, Nicholas J.
dc.contributor.authorFonti, Elio
dc.date.accessioned2011-07-06T15:41:44Z
dc.date.available2011-07-06T15:41:44Z
dc.date.issued2010
dc.description.abstractThe 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.en_UK
dc.identifier.urihttp://dspace.lib.cranfield.ac.uk/handle/1826/5635
dc.language.isoenen_UK
dc.publisherCranfield Universityen_UK
dc.rights© Cranfield University 2010. All rights reserved. No part of this publication may be reproduced without the written permission of the copyright owner.en_UK
dc.titleMeasurements of aircraft wake vortices in ground proximity within an atmospheric boundary layer wind tunnelen_UK
dc.typeThesis or dissertationen_UK
dc.type.qualificationlevelMastersen_UK
dc.type.qualificationnameMasters by Researchen_UK

Files

Original bundle
Now showing 1 - 1 of 1
Thumbnail Image
Name:
Elio_Fonti_Thesis_2010.pdf
Size:
3.63 MB
Format:
Adobe Portable Document Format
Download
License bundle
Now showing 1 - 1 of 1
No Thumbnail Available
Name:
license.txt
Size:
1.79 KB
Format:
Item-specific license agreed upon to submission
Description:
Download

Collections

PhD and Masters by research theses (SoE)