Image:ObliqueShockAngleRelation.png

Size of this preview: 793 × 600 pixels
Full resolution‎ (1,078 × 815 pixels, file size: 38 KB, MIME type: image/png)

[edit] Summary

Description	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.
Source	self-made
Date	created 27th Oct 2007.
Author	-- Myth (Talk) 05:29, 27 October 2007 (UTC)
Permission (Reusing this image)	One is free to use this image. No tags attached.

I, the copyright holder of this work, hereby release it into the public domain. This applies worldwide.

In case this is not legally possible,

I grant any entity the right to use this work for any purpose, without any conditions, unless such conditions are required by law.

Click on a date/time to view the file as it appeared at that time.

	Date/Time	Dimensions	User	Comment
current	05:29, 27 October 2007	1,078×815 (38 KB)	Mythealias (Talk \| contribs)	({{Information\| \|Description = This figure shows the angle at which a 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. )