Title 95-69524 ISBN 0-964 Contents iii PREFACE ACKNOWLEDGMENTS. Cover photograph by Bill Weigand, University of Illinois News Bureau Wind tunnel model (81223} by Yvan Tinel, Tinel Technologies, Northbrook, Illinois First Printing, June 1995 Library of Congress Cataloging in Publication Data Selig, Michael Scott Summary of Low-Speed Airfoil Data, Volume 1 / by Michael Selig, James Guglielmo, Andy Broeren and Philippe Giguere. Broeren, and Philippe Giguere All rights reserved. Horseshoe Circle Virginia Beach, Virginia 23451, USA Copyright © 1995 by MichaelS. Broeren Philippe Giguere Department of Aeronautical and Astronautical Engineering University of Illinois at Urbana-Champaign Summary of Low-Speed Airfoil Data Volume 1 SoarTech Publications Virginia Beach, Virginia SOARTECH PUBLICATIONS 1504 N. His experience with R/C model airplanes comes from his participation in the Society of Automotive Engineer's (S.A.E.) Aero-Design competition from 1991-1994. degree with research in optimization of wind turbine rotors, wind-tunnel boundary-layer corrections and airfoil performance enhancement. Shortly after receiving his Master's degree, he joined the Department of Aeronautical and Astronautical Engineering at the University of Illinois at Urbana-Champaign. PHILIPPE GIGUERE received his Bachelor of Mechanical Engineering degree from McGill University, Montreal, Canada in 1992 and his Master of Science degree from Universite Laval, Quebec, Canada in 1994. His interest in aerodynamics, particularly involving high-lift, low Reynolds number airfoil research, results from several years of participation in the Society of Automotive Engineer's (S.A.E.) Aero-Design competition. Broeren is presently 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 number airfoils. Several months after beginning graduate study in mechanical engineering at the University of Illinois, he joined Prof. BROEREN received his Bachelor of Science degree in Mechanical Engineering from the Milwaukee School of Engineering, Milwaukee, Wisconsin in 1993. Research interests include applied aerodynamics, flight mechanics, and aircraft conceptual/ advanced design. 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 number airfoil aerodynamics. Remaining at the University of Illinois for graduate studies, his research has included such topics as experimental supersonic and subsonic wind-tunnel testing, Magnetic Levitation (MagLev) vehicle design, and the conceptual design of a wing-in-ground-effect aircraft. 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 design. His current research areas include low Reynolds number airfoil aerodynamics, multi-point inverse design of slot suction airfoils, horizontal-axis wind-turbine system design and analysis, and flight simulation. (1992) from the Pennsylvania State University. (1988) from Princeton University and his Ph.D. (1984) from the University of Illinois, his M.S.E. SELIG, an accomplished applied aerodynamicist and airfoil designer, is an Assistant Professor of Aeronautical and Astronautical Engineering at the University of Illinois at Urbana-Champaign. Broeren and Philippe Giguere Volume 1 Summary of Low-Speed Airfoil Data Volume 1 About the Authors DR. Summary of Low-Speed Airfoil Data MichaelS.
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