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Advances in Aerodynamics

Table 1 Comparison of the present results against reference for flow over a cylinder

From: A parallel methodology of adaptive Cartesian grid for compressible flow simulations

 

CL

CD

Strouhal number

Ref1 [36]

0.67

1.39

0.192

Ref2 [37]

0.74

1.32

0.196

CABA

0.69

1.43

0.201

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