UIUC Applied Aerodynamics Group
Current Research Activities

Department of Aeronautical and Astronautical Engineering
University of Illinois at Urbana-Champaign, Urbana, Illinois 61801

Last update 12/6/96
Effects of Boundary Layer Trips on Laminar Separation Bubbles
C.A. Lyon and M.S. Selig
University of Illinois

This case corresponds to the E374 (B) w/ big ZZ trip @ 200k, alpha = 3.28 degs, trip h = 2 layers, trip s/c = 2" in front x/c = 5.54".

Click on image to get an even more detailed look.

This case corresponds to the E374 (B) w/ plain trip @ 200k, alpha = 3.28 degs, trip h =.012", w = 1/8", trip s/c = 0" in front x/c = 5.54"

Click on image to get an even more detailed look.

P.S.: More details of the low Reynolds number airfoil test program can be found here. 10/7/99


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