File:Compressor case from turbojet.jpg

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Summary

Description
English: The low-pressure compressor case from a General Electric J79 turbojet engine. The casing is cut out and the stator blades (sometimes called vanes) are clearly visible. Flow was from left to right: the size of the blades decreases as the air density increases.
Date Taken on 19 July 2011, 15:27:23
Source Own work
Author Olivier Cleynen

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19 July 2011

6 millimetre

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2,234,728 byte

3,648 pixel

2,432 pixel

9b40a7572d9051a81022e4a354709ae5b50fc458

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Date/TimeThumbnailDimensionsUserComment
current13:32, 20 May 2025Thumbnail for version as of 13:32, 20 May 20252,432 × 3,648 (2.13 MB)wikimediacommons>SteinsplitterBotBot: Image rotated by 90°

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