Lo, Kin Hing, Zare-Behtash, Hossein and Kontis, Konstantinos (2015) Flow characteristics along an active jets equipped contour bump in a supersonic freestream and its potential to be applied on transonic aircraft for drag reduction: an experimental study. In 53rd AIAA Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics.. (doi:10.2514/6.2015-1710).
Record type:
Conference or Workshop Item
(Paper)
This record has no associated files available for download.
More information
e-pub ahead of print date: 3 January 2015
Venue - Dates:
53rd AIAA Aerospace Sciences Meeting, , Kissimmee, United States, 2015-01-05 - 2015-01-09
Identifiers
Local EPrints ID: 491702
URI: http://eprints.soton.ac.uk/id/eprint/491702
PURE UUID: 4dde6c41-1209-45e4-b7d8-c06e7bc79313
Catalogue record
Date deposited: 03 Jul 2024 16:10
Last modified: 11 Jul 2024 02:18
Export record
Altmetrics
Contributors
Author:
Kin Hing Lo
Author:
Hossein Zare-Behtash
Author:
Konstantinos Kontis
Download statistics
Downloads from ePrints over the past year. Other digital versions may also be available to download e.g. from the publisher's website.