Combustion Rate of Solid Carbon in the Axisymmetric Stagnation Flowfield Established over a Sphere and/or a Flat Plate
Figure 5
Experimental comparisons for the combustion rate under an atmospheric pressure: (a) in airflow; (b) in CO2-flow with CO2 mass fraction of 0.5; (c) in H2O-flow with H2O mass fraction of 0.5. Data points are experimental [33, 55] and curves are calculated from the theory.
