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Wind-Tunnel Investigation of an NACA 66,2-216 Low-Drag Wing with Split Flaps of Various Sizes, Special Report
| Content Provider | University of North Texas |
|---|---|
| Author | Muse, Thomas C. Neely, Robert H. |
| Organization | Langley Aeronautical Laboratory |
| Description | "An investigation was conducted in the NACA 19-foot pressure wind tunnel of a rectangular wing having NACA 66, 2-216 low-drag airfoil sections and various sizes of simple split flaps. The purpose of the investigation was, primarily, to determine the influence of these flap installations on the aerodynamic characteristics of the wing. Complete lift, drag, and pitching-moment characteristics were determined for a range of test Reynolds numbers from about 2,600,000 to 4,600,000 for each of the installations and for the plain wing" (p. 1). |
| File Format | |
| Archival Resource Key | ark:/67531/metadc65189 |
| Language | English |
| Publisher Date | 2019-01-23 |
| Access Restriction | Open |
| Subject Keyword | aerodynamics airfoils |
| Content Type | Text |
| Resource Type | Report |