File:Compressor case from turbojet.jpg
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Size of this preview: 800 × 533 pixels. Other resolutions: 320 × 213 pixels | 640 × 427 pixels | 1,024 × 683 pixels | 1,280 × 853 pixels | 2,560 × 1,707 pixels | 3,648 × 2,432 pixels.
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Summary[edit]
| 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 | |
| Source | Own work |
| Author | Olivier Cleynen |
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I, the copyright holder of this work, hereby publish it under the following license:
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| Date/Time | Thumbnail | Dimensions | User | Comment | |
|---|---|---|---|---|---|
| current | 07:25, 31 March 2013 | | 3,648 × 2,432 (2.13 MB) | Ariadacapo (talk | contribs) | User created page with UploadWizard |
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