File:TH27G3.jpg
Jump to navigation
Jump to search
Size of this preview: 305 × 598 pixels. Other resolutions: 122 × 240 pixels | 367 × 720 pixels.
Original file (367 × 720 pixels, file size: 23 KB, MIME type: image/jpeg)
Captions
Captions
Add a one-line explanation of what this file represents
Summary[edit]
| 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] |
| Source | US gov |
| Author | US gov |
|
This physics image could be re-created using vector graphics as an SVG file. This has several advantages; see Commons:Media for cleanup for more information. If an SVG form of this image is available, please upload it and afterwards replace this template with
{{vector version available|new image name}}.
It is recommended to name the SVG file “TH27G3.svg”—then the template Vector version available (or Vva) does not need the new image name parameter. |
 | This physics image was uploaded in the JPEG format even though it consists of non-photographic data. This information could be stored more efficiently or accurately in the PNG or SVG format. If possible, please upload a PNG or SVG version of this image without compression artifacts, derived from a non-JPEG source (or with existing artifacts removed). After doing so, please tag the JPEG version with {{Superseded|NewImage.ext}} and remove this tag. This tag should not be applied to photographs or scans. If this image is a diagram or other image suitable for vectorisation, please tag this image with {{Convert to SVG}} instead of {{BadJPEG}}. If not suitable for vectorisation, use {{Convert to PNG}}. For more information, see {{BadJPEG}}. |  |
Licensing[edit]
|
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.
|
 |
Original upload log[edit]
The original description page was here. All following 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 | Thumbnail | Dimensions | User | Comment | |
|---|---|---|---|---|---|
| current | 11:21, 26 March 2007 | | 367 × 720 (23 KB) | Liftarn (talk | contribs) | {{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 |
You cannot overwrite this file.
File usage on Commons
There are no pages that use this file.
File usage on other wikis
The following other wikis use this file:
- Usage on ar.wikipedia.org
- Usage on es.wikipedia.org
- Usage on he.wikipedia.org
- Usage on pt.wikipedia.org
- Usage on ru.wikipedia.org
- Usage on uk.wikipedia.org
