Heat Transfer and Failure Mode Analyses of Ultrahigh-Temperature Ceramic Thermal Protection System of Hypersonic Vehicles
Figure 8
Upper surface temperature at the balance versus (a) surface heat flux and (b) convective heat transfer coefficient. ( in (a) is in KW m−2°C−1 and in (b) is in MW m−2. In (a), = = 20°C at = 0.)
