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 | This is a file from the
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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
|
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.
|
 |
File history
Click on a date/time to view the file as it appeared at that time.
| 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 |
File usage
The following pages on the English Wikipedia use this file (pages on other projects are not listed):
Metadata
Size of this preview:
800 × 466 pixels. Other resolutions:
320 × 186 pixels |
640 × 373 pixels |
1,024 × 596 pixels |
1,280 × 745 pixels |
1,930 × 1,124 pixels.
Original file (1,930 × 1,124 pixels, file size: 502 KB, MIME type: image/png)
| This is a file from the
Wikimedia Commons. Information from its
description page there is shown below. Commons is a freely licensed media file repository. You can help. |
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
|
|
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.
|
|
File history
Click on a date/time to view the file as it appeared at that time.
| 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 |
File usage
The following pages on the English Wikipedia use this file (pages on other projects are not listed):