File:Swept wing w spanwise boundary layer flow.svg

Page contents not supported in other languages.
This is a file from the Wikimedia Commons
From Wikipedia, the free encyclopedia

Original file(SVG file, nominally 531 × 488 pixels, file size: 5 KB)

Summary

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


Licensing

Public domain 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.

Captions

Add a one-line explanation of what this file represents

Items portrayed in this file

depicts

14 August 2008

File history

Click on a date/time to view the file as it appeared at that time.

Date/TimeThumbnailDimensionsUserComment
current09:09, 15 August 2008Thumbnail for version as of 09:09, 15 August 2008531 × 488 (5 KB)Arnero{{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_
No pages on the English Wikipedia use this file (pages on other projects are not listed).

Global file usage

The following other wikis use this file: