"Generating dynamically controllable oscillatory fluid flow"
Bachar T.
United States Patent 6,186,412 February 13, 2001
"Enhanced Performance of Airfoils at Moderate Mach Numbers Using Zero-Mass Flux Pulsed Blowing"
Hites M., Nagib H., Bachar T., Wygnanski, I.
AIAA 2001-0734 39th Aerospace Science Meeting & Exhibit Reno January, 2001
"On the Response of Turbulent Boundary Layer to Concentrated Suction"
Ph.D. Thesis, Tel-Aviv University, 2000.
”Application of Active Separation Control to a Small Unmanned Air Vehicle”
Seifert A., Bachar T., Wygnanski, I., Kariv A., Cohen, H., Yoeli R.,
J. of Aircraft, V36, pp. 474-477, 1999.
"Active Control of Separation in the presence of High Freestream Turbulence
Bachar T., Wygnanski I., David Ashpis D.
APS Meeting Philadelphia, PA November 22-24, 1998
"Lift enhancement using pulsed blowing at compressible flow conditions "
Hites M., Nagib H., Sytsma B.,Wygnanski I., Seifert A., Bachar T.
APS Meeting, San Francisco, November 1997.
"Oscillatory Blowing, a Tool to Delay Boundary Layer Separation"
Seifert A., Bachar T., Koss D., Shepshelovich M. and Wygnanski I.
AIAA J., Vol. 31, No. 11, pp.2052-2060, 1993.
”The Transient Behavior of a Boundary Layer Exposed to Uniform Suction"
Bachar T.
M.Sc. Thesis, Tel-Aviv University, 1992.