File:Supercrit2.jpg

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Supercrit2.jpg(421 × 323 pixels, file size: 11 KB, MIME type: image/jpeg)

Summary[edit]

File information
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)

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(Reusing this file)

See below.



Licensing[edit]

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Date/TimeThumbnailDimensionsUserComment
current16:17, 3 November 2005Thumbnail for version as of 16:17, 3 November 2005421 × 323 (11 KB)Fongs (talk | contribs)philip poppe
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