File:Supercrit2.jpg

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Summary

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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)
Source	Own work ; Diagram/chart prepared by uploader.
Date
Author	Fongs (talk) (Uploads)
Permission (Reusing this file)	See below.

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	Date/Time	Thumbnail	Dimensions	User	Comment
current	16:17, 3 November 2005		421 × 323 (11 KB)	Fongs (talk \| contribs)	philip poppe

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