TY  - CONF

T1  - Prediction of Transition Location and Its Effects on Shock Bump Control on a Natural Laminar Flow Aerofoil

PY  - 2011/06/05

AU  - Deng F

AU  - McIntosh SC

AU  - Qin N

ED  - 

DO  - DOI: 10.1007/978-3-642-25685-1_39

PB  - Springer Berlin Heidelberg

SN  - 9783642256844

SP  - 251

EP  - 256

Y2  - 2024/12/27

ER  -