A New Class of Synthetic Jet Actuators—Part II: Application to Flow Separation Control.

Authors: Gilarranz, J. L., Traub, L. W., Rediniotis, O. K.

Source: Journal of Fluids Engineering; March 2005, Vol. 127 Issue 2, p377-387, 11p

A New Class of Synthetic Jet Actuators—Part I: Design, Fabrication and Bench Top Characterization.

Authors: Gilarranz, J. L., Traub, L. W., Rediniotis, O. K.

Source: Journal of Fluids Engineering; March 2005, Vol. 127 Issue 2, p367-376, 10p

Alleviation of pitch-up on delta wings using distributed porosity.

Authors: Traub, L. W., Moeller, B., Galls, S. F.

Source: Aeronautical Journal; July 1999, Vol. 103 Issue 1025, p339-347, 9p

Predicition of tunnel wall upwash for delta wings including vortex breakdown effects.

Authors: Traub, L. W.

Source: Aeronautical Journal; March 1999, Vol. 103 Issue 1021, p139-142, 4p

Application of the vortex breakdown phenomenon in the attenuation of trailing vortices.

Authors: Traub, L. W., Mani, S., Galls, S. F.

Source: Aeronautical Journal; December 1998, Vol. 102 Issue 1018, p439-444, 6p

Efficient lift enhancement of a blunt edged delta wing.

Authors: Traub, L. W.

Source: Aeronautical Journal; November 1997, Vol. 101, p439-445, 7p

Effects of delta planform tip sails on the performance of a blunt edged rectangular wing.

Authors: Traub, L. W.

Source: Aeronautical Journal; February 1997, Vol. 101, p87-92, 6p

Analytic prediction of vortex drag of high aspect ratio tapered wings.

Authors: Traub, L. W.

Source: Aeronautical Journal; January 1997, Vol. 101, p25-27, 3p

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