Combustion Rate of Solid Carbon in the Axisymmetric Stagnation Flowfield Established over a Sphere and/or a Flat Plate
Figure 8
Combustion rate as a function of the surface temperature, with the H2O mass-fraction taken as a parameter. Data points are combustion rate measured in the axisymmetric stagnation airflow over a flat plate [38, 64]; curves are calculated by use of the explicit combustion-rate expressions.
