A Numerical Scheme Based on an Immersed Boundary Method for Compressible Turbulent Flows with Shocks: Application to Two-Dimensional Flows around Cylinders

Table 2

Test cases.

Re	Mach	Scheme	Mesh size	Case
300	0.3	A (10)	0.2D	M03-A-0200D
			0.1D	M03-A-0100D
			0.05D	M03-A-0050D
			0.025D	M03-A-0025D
		B ((10) and MUSCL-Roe [22, 23] for nearby body)	0.2D	M03-B-0200D
			0.1D	M03-B-0100D
			0.05D	M03-B-0050D
			0.025D	M03-B-0025D
		C (MUSCL-Roe [22, 23])	0.2D	M03-C-0200D
			0.1D	M03-C-0100D
			0.05D	M03-C-0050D
			0.025D	M03-C-0025D
300	1.2	A (10)	0.2D	M12-A-0200D
			0.1D	M12-A-0100D
			0.05D	M12-A-0050D
			0.025D	M12-A-0025D
		B ((10) and MUSCL-Roe [22, 23] for nearby body)	0.2D	M12-B-0200D
			0.1D	M12-B-0100D
			0.05D	M12-B-0050D
			0.025D	M12-B-0025D
		C (MUSCL-Roe [22, 23])	0.2D	M12-C-0200D
			0.1D	M12-C-0100D
			0.05D	M12-C-0050D
			0.025D	M12-C-0025D
300	2.0	A (10)	0.2D	M20-A-0200D
			0.1D	M20-A-0100D
			0.05D	M20-A-0050D
			0.025D	M20-A-0025D
		B ((10) and MUSCL-Roe [22, 23] for nearby body)	0.2D	M20-B-0200D
			0.1D	M20-B-0100D
			0.05D	M20-B-0050D
			0.025D	M20-B-0025D
		C (MUSCL-Roe [22, 23])	0.2D	M20-C-0200D
			0.1D	M20-C-0100D
			0.05D	M20-C-0050D
			0.025D	M20-C-0025D