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Summary
| Description |
English: With differential ailerons, one aileron is raised a greater distance than the other aileron and is lowered for a given movement of the control wheel or control stick. This produces an increase in drag on the descending wing. The greater drag results from deflecting the up aileron on the descending wing to a greater angle than the down aileron on the rising wing. While adverse yaw is reduced, it is not eliminated completely. |
| Date | |
| Source | Pilot's Handbook of Aeronautical Knowledge, page 6-4 |
| Author | Federal Aviation Administration |
Licensing
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This image or file is a work of a Federal Aviation Administration employee, taken or made as part of that person's official duties. As a work of the U.S. federal government, the image is in the public domain in the United States.
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File history
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| Date/Time | Thumbnail | Dimensions | User | Comment | |
|---|---|---|---|---|---|
| current | 03:14, 14 April 2023 | | 1,930 × 1,124 (502 KB) | 痛 | Uploaded a work by {{label|Q335357}} from Pilot's Handbook of Aeronautical Knowledge, page 6-4 with UploadWizard |
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