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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.
Summary of Low-Speed Airfoil Data – Volume 5 represents the fifth installment in a series of books doc-umenting the ongoing work of the University of Illinois at Urbana-Champaign Low-Speed Airfoil Tests (UIUC LSATs). The project’s purpose remains unchanged since the original work was performed and doc-
0 5 Summary of Low-Speed Airfoil Data 0 7 0 2 0 0 0 8 0 6 a 0 4 0 2 0 0 0 6 0 2. Table 4.1: Test Matrix and Run Number Index. Model (Builder) Designer. Configuration. V-dist & Profile.
Low Reynolds number airfoils were designed for high lift-to-drag ratios. Design considerations of low Re-airfoils are discussed and design examples are presented. It is shown that the performance of …
Abstract. Wind tunnel data on 37 airfoils tested at Reynolds Numbers ranging from 60,000 to 500,000. Library availability. Discover UIUC Full Text. Fingerprint. Dive into the research topics of 'Summary of Low Speed Airfoil Data: Volume 3'. Together they form a unique fingerprint. View full fingerprint. Cite this. APA. Standard. Harvard. Vancouver.
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. Standard. Harvard. Vancouver.
