VORTICITY IN A FORCED WALL JET
Drs. Miguel Visbal and Datta Gaitonde
U. S. Air Force Research Laboratory at Wright-Patterson Air Force Base, Dayton, Ohio
The image displays the iso-surface of vorticity magnitude in a forced wall
jet obtained using direct high-order numerical simulations (DNS).
References:
1) M. Visbal, D. Gaitonde, and S. Gogineni
"Direct Numerical Simulation of a Forced Transitional Plane Wall Jet,"
29th AIAA Fluid Dynamics Conference, Albuquerque, NM, June 1998 (AIAA
98-2643).
2)S. Gogineni, M. Visbal, D. Gaitonde, and C. Shih "Analysis
of flow transition in an acoustically excited wall jet," Proceedings of
the 3rd ASME/JSME Fluid Engineering Conference, San Francisco, CA, July
1999 (FEDSM99-6959)