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A numerical study has been conducted to examine the turbulent heat transfer of a nanofluid, methane-CuO, in a circular cooling tube at a supercritical pressure of 8MPa, a phenomenon relevant to the rocket engine cooling application. Results reveal that at a surface heat flux of 3MW/m2 and an inlet flow velocity of 25m/s, the addition of nanoparticles decreases the heat transfer rate, dictated by significant...
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