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The parameter values express material opacity as a power-law of material temperature and density.
Variations of maximum specific thrust with freestream Mach numbers and material temperature limit are analyzed respectively.
The effects of angle, material, temperature, and humidity on climbing ability were also discussed.
The prediction of the average moisture content and material temperature compared favourably with the experimental results.
Despite the destruction reconstruction process, the material temperature is below its melting point.
However, the maximum material temperature and the maximum thermal stress occur at the trailing edge near the mid-span.
However, the strength of the material is reduced because the material temperature reaches the recrystallization temperature during hot working.
These include all material temperature limits allowing 500 875 °C in the breeder zone to promote tritium release.
Most part of this irreversible energy is dissipated as heat and consequently the material temperature increases.
In constructing the scheme, one has the freedom to choose between expanding the material temperature, or the equivalent black body radiation energy density at the material temperature, in terms of finite element basis functions.
This observation raises the question of the influence of material temperature on the response of flames to acoustic perturbations.
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