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θ-β-M Diagram

Creator: Philipp Dobler (original)

In supersonic flow shock waves can occur due to small disturbances of the flow. A θ-β-M Diagram shows the relations between the deflection angle θ, the shock angle β and the Mach number M for an oblique shock.


θ-β-M Diagram

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  theta-beta-m-diagram.typ (368 lines)