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Free-Spinning-Tunnel Tests of a 1/24-Scale Model of the Grumman XF9F-2 Airplane, TED No. NACA DE 317
| Content Provider | University of North Texas |
|---|---|
| Author | Berman, Theodore |
| Organization | Langley Aeronautical Laboratory |
| Organization | United States. Department of the Navy. Bureau of Aeronautics. |
| Description | "An investigation of the spin and recovery characteristics of a scale model of the Grumman XF9F-2 airplane has been conducted in the Langley 20-foot free-spinning tunnel. The effects of control settings and movements on the erect and inverted spin and recovery characteristics of the model in the flight loading were determined. The investigation also included spin-recovery-parachute, pilot-escape, and rudder-pedal- . force tests" (p. 1). |
| File Format | |
| Archival Resource Key | ark:/67531/metadc64607 |
| Language | English |
| Publisher Date | 2018-12-20 |
| Access Restriction | Open |
| Subject Keyword | Grumman XF9F-2 spinning characteristics |
| Content Type | Text |
| Resource Type | Report |