This picture displays the iso-surface of vorticity magnitude in a forced wall
jet which was obtained using direct high-order numerical simulations (DNS).
The computations were performed by Dr. Miguel Visbal and Dr. Datta Gaitonde
of U.S. Air Force Research Laboratory at Wright-Patterson Air Force Base
located in Dayton, Ohio. For further information on this work please refer
the following papers.
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)
