Research Article
Magnetohydrodynamic Simulations of Hypersonic Flow over a Cylinder Using Axial- and Transverse-Oriented Magnetic Dipoles
Table 1
Percent changes in
, average wall-adjacent temperature, and shock-standoff distance for various
.
| Case | | Average wall-adjacent temperature | Shock distance |
| 0.2 T -oriented | −5.0% | −3.2% | 0.14% | 1 T -oriented | −11.7% | −13.5% | 1.5% | 2 T -oriented | −17.0% | −18.5% | 5.4% | 0.2 T -oriented | −3.0% | −1.1% | 0.10% | 1 T -oriented | −4.7% | −10.1% | 1.2% | 2 T -oriented | −3.7% | −17.5% | 4.5% |
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