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Advances in Aerodynamics

Table 3 Comparison of the present results against reference for supersonic flow around a sphere

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

 

θ

L

Ls

Ref [38]

150.0

0.36

0.20

Ref [44]

150.9

0.38

-

CABA

150.6

0.40

0.20

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