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International Journal of Aerospace Engineering
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2021
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Article
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Tab 1
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Research Article
Magnetohydrodynamic Control of Hypersonic Separation Flows
Table 1
Freestream conditions for compression corner flow.
Property
Symbol
Value
Mach number
Ma
14.1
Temperature
T
∞
72.7 K
Reynolds number
Re/m
Density
ρ
∞