TY  - CONF

T1  - 3D bumps for transonic wing shock control and drag reduction

CY  - London

JO  - CD-ROM

UR  - http://eprints.whiterose.ac.uk/86394/

PY  - 2002/06/10

AU  - Qin N

AU  - Monet D

AU  - Shaw ST

ED  - 

PB  - Royal Aeronautical Society

SN  - 978-1857681970

Y2  - 2024/12/27

ER  -