Qin, N., Monet, D. and Shaw, S.T. (2002) 3D bumps for transonic wing shock control and drag reduction. In: CEAS Aerospace Aerodynamics Research Conference. CEAS Aerospace Aerodynamics Research Conference, 10-12 Jun 2002, Cambridge, UK. Cat no. 439 . Royal Aeronautical Society ISBN 1857681975
Metadata
| Item Type: | Proceedings Paper |
|---|---|
| Authors/Creators: |
|
| Copyright, Publisher and Additional Information: | © 2002 The Author(s) |
| Dates: |
|
| Institution: | The University of Sheffield |
| Academic Units: | The University of Sheffield > Faculty of Engineering (Sheffield) > Department of Mechanical Engineering (Sheffield) |
| Depositing User: | Symplectic Sheffield |
| Date Deposited: | 09 Oct 2015 14:16 |
| Last Modified: | 19 Dec 2022 13:31 |
| Published Version: | http://aerosociety.com/News/Proceedings |
| Status: | Published |
| Publisher: | Royal Aeronautical Society |
| Series Name: | Cat no. 439 |
| Open Archives Initiative ID (OAI ID): | oai:eprints.whiterose.ac.uk:86394 |
Download not available
A full text copy of this item is not currently available from White Rose Research Online
CORE (COnnecting REpositories)
CORE (COnnecting REpositories)