A backscatter laser Doppler velocimeter which simultaneously senses the axial and the tangential components of the velocity has been used to measure the velocity distributions in the near wake of a swept wing semispan transport model in a wind tunnel. The model configuration included nacelles, pylons, antishock bodies, and wing flaps which could be deflected 27 deg. Typical wake vortex velocity profiles are presented for the flaps-retracted and the flaps-deployed 27 deg configurations, respectively.
Vortex measurements behind a swept wing transport model
Journal of Aircraft ; 11
01.06.1974
Sonstige
Keine Angabe
Englisch
Vortex Measurements Behind a Swept Wing Transport Model
AIAA | 1974
|Near-field tip vortex behind a swept wing model
Tema Archiv | 2006
|Vortex Wake Generated Behind a Forward Swept Wing
AIAA | 2009
|Vortex Wake Generated Behind a Forward Swept Wing
Online Contents | 2009
|RECEPTIVITY MEASUREMENTS ON A SWEPT-WING MODEL
British Library Conference Proceedings | 2011
|