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| Keywords: ObliqueShockAngleRelation.png 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 own original text self-made 1 created 27th Oct 2007 -- Myth <small> Talk </small> 05 29 27 October 2007 UTC One is free to use this image No tags attached Mythealias Original upload log en wikipedia ObliqueShockAngleRelation png wikitable - 2007-10-27 05 29 1078×815× 38726 bytes Mythealias 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 Oblique shock waves | ||||
