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File:ObliqueShockAngleRelation.png

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Summary

Description
English: This figure shows the angle at which a shock will be formed in a 2D supersonic flowfield for various deflection angle. M1 is the upstream Mach number, M2 is the downstream Mach number.
Date
Source Own work (Original text: self-made)
Author -- Myth (Talk) 05:29, 27 October 2007 (UTC)
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Public domain This work has been released into the public domain by its author, Mythealias at English Wikipedia. This applies worldwide.
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Date/Time Dimensions User Comment
2007-10-27 05:29 1078×815× (38726 bytes) Mythealias {{Information| |Description = This figure shows the angle at which a [[oblique shock|shock]] will be formed in a 2D supersonic flowfield for various deflection angle. M<sub>1</sub> is the upstream Mach number, M<sub>2</sub> is the downstream Mach number.

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Date/TimeThumbnailDimensionsUserComment
current18:46, 8 November 2016Thumbnail for version as of 18:46, 8 November 20161,078 × 815 (38 KB)StevenliuyiTransferred from en.wikipedia

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