Of wind-tunnel tests conducted at Princeton University on over 60 airfoils for Which was first published as SoarTech 8 in 1989. The companion book Airfoils at Low Speeds (by Selig, Donovan and Fraser), WIND- TUNNEL FACILITY AND MEASUREMENT TECHNIQUESĪ reader just discovering airfoil aerodynamics will find it helpful to reference James Guglielmo, Andy Broeren and Philippe Giguere.ġ. Summary of Low-Speed Airfoil Data, Volume 1 / by Michael Selig, Library of Congress Cataloging in Publication Data Wind tunnel model (81223} by Yvan Tinel, Tinel Technologies, Northbrook, Illinois Broeren, and Philippe GiguereĬover photograph by Bill Weigand, University of Illinois News Bureau University of Illinois at Urbana-Champaign He also flies full-scale gliders.ĭepartment of Aeronautical and Astronautical Engineering His experience with R/C model airplanes comes from his participation in the Society of Automotive Engineer's (S.A.E.) Aero-Design competition fromġ991-1994. In optimization of wind turbine rotors, wind-tunnel boundary-layer corrections and airfoil The Department of Aeronautical and Astronautical Engineering at the University of Illinois at Urbana-Champaign. Shortly after receiving his Master's degree, he joined University, Montreal, Canada in 1992 and his Master of Science degree from Universite PHILIPPE GIGUERE received his Bachelor of Mechanical Engineering degree from McGill Research, results from several years of participation in the Society of Automotive Engineer's His interest in aerodynamics, particularly involving high-lift, low Reynolds number airfoil Working toward a Master of Science degree with thesis research in unsteady fluid mechanics. In addition to continuing work in this area, Mr.
Guglielmo in their efforts to establish a program for testing low Reynolds Several months afterīeginning graduate study in mechanical engineering at the University of Illinois, he joined The Milwaukee School of Engineering, Milwaukee, Wisconsin in 1993. BROEREN received his Bachelor of Science degree in Mechanical Engineering from Research interests include applied aerodynamics, flight mechanics, and aircraft conceptual/ advanced design.ĪNDY P. Guglielmo is also the co-founder and present coordinator of the UIUC Low-Speed Airfoil Tests and is working toward a Master of Science degree in experimental low Reynolds (MagLev) vehicle design, and the conceptual design of a wing-in-ground-effect aircraft.
Topics as experimental supersonic and subsonic wind-tunnel testing, Magnetic Levitation Remaining at the University of Illinois for graduate studies, his research has included such GUGLIELMO received his Bachelor of Science degree in Aeronautical and Astronautical Engineering from the University of Illinois at Urbana-Champaign in May 1992. He teaches courses in applied aerodynamics and aircraft
Multi-point inverse design of slot suction airfoils, horizontal-axis wind-turbine system designĪnd analysis, and flight simulation. His current research areas include low Reynolds number airfoil aerodynamics, (1988) from Princeton University and his Ph.D. (1984) from the University of Illinois, his SELIG, an accomplished applied aerodynamicist and airfoil designer, isĪn Assistant Professor of Aeronautical and Astronautical Engineering at the University of
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