International Journal of Aerospace Engineering / 2010 / Article / Fig 6

Research Article

Behavior of Carbon-Carbon Composite under Intense Heating

Figure 6

Surface temperature versus time ( 𝑞 = 0 . 4 5 W / m m 2 , 𝑢 = 1 9 0 0 0 c m / s ) .
257957.fig.006

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