File:Swept wing w spanwise boundary layer flow.svg
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Size of this PNG preview of this SVG file: 531 × 488 pixels. Other resolutions: 261 × 240 pixels | 522 × 480 pixels | 836 × 768 pixels | 1,114 × 1,024 pixels | 2,229 × 2,048 pixels.
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| Description |
English: in the subsonic, mostly at landing and take off, the swept wing on the rear side has a spanwise flow of its boundary layer. |
| Date | |
| Source | Own work |
| Author | Arnero |
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I, the copyright holder of this work, release this work into the public domain. This applies worldwide. In some countries this may not be legally possible; if so: I grant anyone the right to use this work for any purpose, without any conditions, unless such conditions are required by law. |
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| Date/Time | Thumbnail | Dimensions | User | Comment | |
|---|---|---|---|---|---|
| current | 09:09, 15 August 2008 | | 531 × 488 (5 KB) | Arnero (talk | contribs) | {{Information |Description={{en|1=in the subsonic, mostly at landing and take off, the swept wing on the rear side has a spanwise flow of its boundary layer.}} |Source=Own work by uploader |Author=Arnero |Date=20080814 |Permission= |other_ |
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