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Free-Spinning-Tunnel Tests of a 1/16-Scale Model of the Chance Vought XF5U-1 Airplane, TED No. NACA 2349
| Content Provider | University of North Texas |
|---|---|
| Author | White, Richard P. |
| Organization | Langley Aeronautical Laboratory |
| Organization | United States. Department of the Navy. Bureau of Aeronautics. |
| Description | "Spin tests of a 1/16-scale model of the Chance Vought XF5U-1 airplane have been performed in the Langley 20-foot free-spinning tunnel. The effect of control position and movement upon the erect and inverted spin and recovery characteristics as well as the effects of propellers, of stability flaps, and of various revisions to the design configuration have been determined for the normal fighter loading. The investigation also included spin recovery parachute, tumbling, and pilot-escape tests" (p. 1). |
| File Format | |
| Archival Resource Key | ark:/67531/metadc64197 |
| Language | English |
| Publisher Date | 2018-12-20 |
| Access Restriction | Open |
| Subject Keyword | Chance Vought XF5U-1 spinning characteristics |
| Content Type | Text |
| Resource Type | Report |
