Image:TH27G3.jpg
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| This is a file from the Wikimedia Commons. The description on its description page there is shown below.
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| Description |
Airplane with static dynamic stability. Static en:directional stability. In an equilibrium condition (figure (a)), an airplane flies so that the en:yaw angle is zero. To have static directional stability, the appropriate positive or negative yawing moment should be generated to compensate for a negative or positive en:sideslip angle excursion. Credits - NASA Source: [1] |
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| Source |
Originally from en.wikipedia; description page is/was here. |
| Date |
2007-01-21 (original upload date) |
| Author |
Original uploader was Dhaluza at en.wikipedia |
| Permission (Reusing this image) |
PD-USGOV-FAA. |
[edit] License information
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This image is a work of a Federal Aviation Administration employee, taken or made during the course of an employee's official duties. As works of the U.S. federal government, all FAA images are in the public domain. |  |
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[edit] Original upload log
(All user names refer to en.wikipedia)
- 2007-01-21 20:42 Dhaluza 367×720×8 (23076 bytes) Airplane with static dynamic stability. Static [[directional stability]]. In an equilibrium condition (figure (a)), an airplane flies so that the [[yaw angle]] is zero. To have static directional stability, the appropriate positive or negative yawing mom
File history
Click on a date/time to view the file as it appeared at that time.
| Date/Time | Dimensions | User | Comment | |
|---|---|---|---|---|
| current | 11:21, 26 March 2007 | 367×720 (23 KB) | Liftarn | ({{Information |Description=Airplane with static dynamic stability. Static en:directional stability. In an equilibrium condition (figure (a)), an airplane flies so that the en:yaw angle is zero. To have static directional stability, the appropri) |
