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File:Polar diagram of coefficients of lift and drag for angles of attack.png

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Polar_diagram_of_coefficients_of_lift_and_drag_for_angles_of_attack.png (720 × 540 pixels, file size: 66 KB, MIME type: image/png)

Summary

Description
English: Polar diagram of coefficients of lift (CL) and drag (CD) for the angles of attack shown for a hypothetical sail. The dotted line is tangential with the point of highest ratio of lift over drag (CL / CD). Also shown is flow status, ranging from attached to stalled.
Date
Source Own work
Author HopsonRoad

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4 April 2015

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Date/TimeThumbnailDimensionsUserComment
current17:32, 6 April 2015Thumbnail for version as of 17:32, 6 April 2015720 × 540 (66 KB)HopsonRoadShow flow status.
21:18, 4 April 2015Thumbnail for version as of 21:18, 4 April 2015720 × 540 (57 KB)HopsonRoadAxes, tick marks
18:15, 4 April 2015Thumbnail for version as of 18:15, 4 April 2015720 × 540 (54 KB)HopsonRoadUser created page with UploadWizard

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