Cover Picture: ZAMM 6–7 / 2013


Abstract

See in this issue, pages 387–402: Triangulation at time t = 0 with 45856 elements used for the computation of hypersonic flow and its detail near the airfoil; Mach number distribution at time instants t = 0.00058 s for the far-field velocity 680 m/s M = 2.0) and Reynolds numbers Re = 107

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