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Mathematical Problems in Engineering
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Mathematical Problems in Engineering
/
2020
/
Article
/
Fig 10
/
Research Article
On Asymptotic Behavior of HLL-Type Schemes at Low Mach Numbers
Figure 10
Upwall pressure coefficient
for NACA0012 airfoil. (a) Ma
0
= 0.0001. (b) Ma
0
= 0.01. (c) Ma
0
= 0.1.
(a)
(b)
(c)