The Development of Crossflow Vortices on a 45 Degree Swept Wing Arizona State University

Format:

Conference/Event

Author/Creator:

Mousseux, Marc C., author.

Conference Name:

Aerospace Technology Conference & Exposition (1989-09-25 : Anaheim, California, United States)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1989

Summary:

Three-dimensional boundary-layer experiments are currently being conducted on a 45° swept wing in the Arizona State University Unsteady Wind Tunnel. Crossflow-dominated transition is produced via a model with contoured end liners to simulate infinite swept-wing flow. Fixed-wavelength stationary and travelling crossflow vortices are observed. The stationary vortex wavelengths vary with Reynolds number as predicted by linear-stability theory but with observed wavelengths which are about 25% smaller than theoretically predicted. The frequencies of the most-amplified moving waves are in agreement with linear-stability theory; travelling waves at higher frequencies than predicted are also observed. These higher-frequency waves may be harmonics of the primary crossflow waves generated by a parametric resonance phenomena. Boundary-layer profiles measured at several spanwise locations show streamwise disturbance profiles characteristic of the crossflow instability. Near the transition location severe distortions of the laminar boundary-layer profiles are observed. Mean-profile measurements are compared to theoretical predictions

Notes:

Vendor supplied data

Publisher Number:

892245

Access Restriction:

Restricted for use by site license