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Advances in Aerodynamics

Table 3 Position of separation point xs and reattachment point xr on leading-edge compressible ramp

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

Tw

xs

xr

300 K

0.84

1.20

400 K

0.81

1.25

500 K

0.77

1.31

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