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Summary of Low-Speed Airfoil Data is only the first in what should be a series of volumes that document the ongoing low Reynolds number airfoil tests at the University of Illinois at Urbana-Champaign. In this volume, the airfoils tested cover a broad spectrum that includes airfoils for free flight model aircraft, heavy
Summary of Low-Speed Airfoil Data, Volume 2 is the second book in the se ries that documents the ongoing work of the University of Illinois at Urbana Champaign Low-Speed Airfoil Tests (UIUC LSATs) program.
It is our intention for Summary of Low-Speed Airfoil Data – Volume 5 to follow closely the format of the previous volumes making the current installment easy to navigate for those familiar with the series. As before, Chapter 1 discusses the scope of the current tests and briefly describes the airfoils and configurations tested.
The goals of the UIUC Low-Speed Airfoil Tests (UIUC LSATs) program are to design, analyze and wind tunnel test airfoils for low Reynolds number applications. The UIUC Applied Aerodynamics group has been a leader in this research area with new airfoil designs being applied to unmanned aerial vehicles, small wind turbines, model aircraft and many ...
Overview. Fingerprint. Abstract. Wind tunnel data on 25 airfoils tested at Reynolds Numbers ranging from 40,000 to 400,000. Library availability. Discover UIUC Full Text. Fingerprint. Dive into the research topics of 'Summary of Low-Speed Airfoil Data: Volume 2'. Together they form a unique fingerprint. View full fingerprint. Cite this. APA.
1 maj 1996 · Multi-Objective Optimization and Optimal Airfoil Blade Selection for a Small Horizontal-Axis Wind Turbine (HAWT) for Application in Regions with Various Wind Potential. The type of airfoil with small wind turbine blades should be selected based on the wind potential of the area in which the turbine is used.
Dive into the research topics of 'Summary of Low Speed Airfoil Data: Volume 3'. Together they form a unique fingerprint.
