For absolute chamber gas temperature Tg, absolute liquid temperature Tl, absolute wall temperature on the gas side of the wall Twg, overall film coefficient h, gas film coefficient hg and liquid film coefficient hl, determine the expression for heat transferred per unit area q.

For absolute chamber gas temperature Tg, absolute liquid temperature Tl, absolute wall temperature on the gas side of the wall Twg, overall film coefficient h, gas film coefficient hg and liquid film coefficient hl, determine the expression for heat transferred per unit area q. Correct Answer q = hg (To – Twg)

q = hg (To – Twg) is the correct expression for heat transferred per unit area q. This is true for a regeneratively cooled thrust chamber. The strength of the material as well as its thermal properties are considered to be a function of temperature.

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