Magnetohydrodynamic Simulations of Hypersonic Flow over a Cylinder Using Axial- and Transverse-Oriented Magnetic Dipoles

Table 1

Percent changes in 𝐶_𝑑, average wall-adjacent temperature, and shock-standoff distance for various 𝐵_max.

Case	𝐶𝑑	Average wall-adjacent temperature	Shock distance
0.2 T 𝑋-oriented	−5.0%	−3.2%	0.14%
1 T 𝑋-oriented	−11.7%	−13.5%	1.5%
2 T 𝑋-oriented	−17.0%	−18.5%	5.4%
0.2 T 𝑌-oriented	−3.0%	−1.1%	0.10%
1 T 𝑌-oriented	−4.7%	−10.1%	1.2%
2 T 𝑌-oriented	−3.7%	−17.5%	4.5%