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Advances in Aerodynamics

Table 1 L2 norm error and order of accuracy for the manufactured solution case

From: On the investigation of shock wave/boundary layer interaction with a high-order scheme based on lattice Boltzmann flux solver

P

Mesh size h

L2 error

Order

2

1/10

3.40e-4

–

1/16

8.08e-5

3.05

1/32

1.02e-5

2.98

1/64

1.34e-6

2.92

3

1/10

2.32e-5

–

1/16

3.51e-6

4.02

1/32

2.18e-7

4.09

1/64

1.61e-8

3.75

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