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The average heat fluxes from the heated wall were predicted using the present empirical correlations and the maximum heat flux at p/h=10 reached ≈1.5 MW/m2 at Re=65 000.
A reduction of about 36% in maximum heat flux at Mach 3.0 and about 21% at Mach 7.0 compared to the maximum heat flux for CEV was observed.
Maximum heat flux position and its propagation velocity are plotted as a function of time.
It is demonstrated that increase in water velocity decreases the maximum heat flux and delays the wetting front movement.
For the fuels in the upper stack, the maximum heat flux was found at the CAR located at 650 mm.
The maximum heat flux to JT-60SA divertor is estimated to ∼15 MW/m2 for 100 s.
For the fuels in the lower stack, the maximum heat flux was found at the CAR located at 450 mm.
To characterize multiple functionalities, objective equations are formulated for density, compressive modulus, compressive strength, and maximum heat flux.
The key normalisation variables are the duration of the heat input and the maximum heat flux density.
Maximum heat flux on the cooling channel surface is defined as the objective function in the optimization process.
Numerical simulations show that blunting the leading edge could reduce the maximum heat flux effectively, but it also degrades the aerodynamic performances.
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