File:Supercrit2.jpg
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Summary
<templatestyles src="Information/styles.css"/>
| Description |
Supercritical airfoil Mach Number/pressure coefficient diagram. The sudden increase in pressure coefficient at midchord is due to the shock. (y-axis:Mach number (or pressure coefficient, negative up); x-axis: position along chord, leading edge left) |
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| Source |
Template:Own ; Diagram/chart prepared by uploader. |
| Date | |
| Author | |
| Permission (Reusing this file) |
See below.
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Licensing
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