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Wing loads on the Bell X-1 research airplane (10 percent thick wing) as determined by pressure-distribution measurements in flight at subsonic and transonic speeds
| Content Provider | University of North Texas |
|---|---|
| Author | Knapp, Ronald J. Jordan, Gareth H. |
| Organization | Langley Aeronautical Laboratory |
| Description | Report presenting measurements of wing loads made on the left wing of the Bell X-1 research airplane. Data are presented within a wing-panel normal-force coefficient and Mach number range. Results regarding span load distributions, wing-panel aerodynamic characteristics, and wing-to-fuselage carry over are provided. |
| File Format | |
| Archival Resource Key | ark:/67531/metadc59667 |
| Language | English |
| Publisher Date | 2018-06-27 |
| Access Restriction | Open |
| Subject Keyword | Bell X-1 aircraft wings |
| Content Type | Text |
| Resource Type | Report |