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Tabulated pressure data for several flap-type trailing edge controls on a trapezoidal wing at Mach numbers of 1.61 and 2.01
| Content Provider | University of North Texas |
|---|---|
| Author | Lord, Douglas R. Czarnecki, K. R. |
| Organization | Langley Aeronautical Laboratory |
| Description | Report presenting an investigation at two Mach numbers for a range of Reynolds numbers to determine the pressure distributions at several spanwise stations for a series of 25.4-percent-chord trailing-edge controls on a trapezoidal wing with a 23 degree sweptback leading edge, aspect ratio of 3.1, and taper ratio of 0.4. The report contains the tabulated pressure data for the complete range of test variables. |
| File Format | |
| Archival Resource Key | ark:/67531/metadc62004 |
| Language | English |
| Publisher Date | 2018-05-01 |
| Access Restriction | Open |
| Subject Keyword | pressure distributions aircraft control aircraft wings |
| Content Type | Text |
| Resource Type | Report |