File:GaTurbineBlade.svg

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Original file(SVG file, nominally 545 × 298 pixels, file size: 203 KB)

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Summary

Description
English: A schematic of a high-pressure turbine blade as used in aircraft jet engines. An internal cooling system enables a temperature gradient across the walls of the blade. Cooling holes allow the cooling air to exit and cover the outer blade surface with a cooling film.
Date
Source Own work by uploader; produced with Adobe illustrator
Author Tomeasy

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GNU head Permission is granted to copy, distribute and/or modify this document under the terms of the GNU Free Documentation License, Version 1.2 or any later version published by the Free Software Foundation; with no Invariant Sections, no Front-Cover Texts, and no Back-Cover Texts. A copy of the license is included in the section entitled GNU Free Documentation License.
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17 February 2009

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Date/TimeThumbnailDimensionsUserComment
current05:15, 17 February 2009Thumbnail for version as of 05:15, 17 February 2009545 × 298 (203 KB)imagescommonswiki>Tomeasy{{Information |Description={{en|1=A high-pressure turbine blade with internal cooling as used in aircraft jet engines.}} |Source=Own work by uploader; produced with Adobe illustrator |Author=Tomeasy |Date=2009-02-17 |Permission= |other_ve

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