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Investigation of a trailing-edge paddle-control surface on a triangular wing of aspect ratio 2 at subsonic and supersonic speeds
| Content Provider | University of North Texas |
|---|---|
| Author | Ball, Louis H. |
| Organization | Ames Aeronautical Laboratory (U.S.) |
| Description | Report presenting an experimental investigation of external airfoils, known as paddle-control surfaces, as the longitudinal control device on a triangular wing of aspect ratio 2. The lift, drag, pitching moment, and hinge moment were obtained for a variety of Mach numbers. |
| File Format | |
| Archival Resource Key | ark:/67531/metadc59911 |
| Language | English |
| Publisher Date | 2018-06-15 |
| Access Restriction | Open |
| Subject Keyword | aircraft control airfoils |
| Content Type | Text |
| Resource Type | Report |