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Advances in Aerodynamics
Fig. 6 | Advances in Aerodynamics

Fig. 6

From: A brief review on the convergence to steady state solutions of Euler equations with high-order WENO schemes

Fig. 6

The numerical solution of the 1D steady shock wave with Mach number M∞=2 using the fifth-order WENO scheme with the new smoothness indicator (39). Left: zoomed density distribution downstream of the shock wave and its comparison with the traditional WENO scheme. WENO-JS represents the numerical result of the traditional WENO scheme [6]. WENO-ZS represents the result from the WENO scheme with the new smoothness indicator. Right: the time evolution of the average residue of WENO-ZS

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