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Effect of Changes in Aileron Rigging on the Stick Forces of a High-Speed Fighter Airplane
| Content Provider | University of North Texas |
|---|---|
| Author | Murray, Harry E. Warren, S. Anne |
| Organization | Langley Aeronautical Laboratory |
| Description | "The effects of changes in aileron rigging between 2 deg up and 2 deg down on the stick forces were determined from wind-tunnel data for a finite-span wing model. These effects were investigated for ailerons deflecting equally in both directions and linearly with stick deflection. Data were analyzed for a Frise, a sealed internally balanced, and a beveled-trailing-edge aileron" (p. 1). |
| File Format | |
| Archival Resource Key | ark:/67531/metadc61638 |
| Language | English |
| Publisher Date | 2019-01-08 |
| Access Restriction | Open |
| Subject Keyword | ailerons aileron rigging stick force characteristics |
| Content Type | Text |
| Resource Type | Report |