Numerical Investigation of an Axisymmetric Model Scramjet Assisted with Cavity of Different Aft Wall Angles

<div>Mass fraction of C<sub>2</sub>H<sub>4</sub> at different lines in the jet plane; the black dashed line is cavity lip, and the red solid line is fuel boundary where the mass fraction of C<sub>2</sub>H<sub>4</sub> equals 0.01.</div>

International Journal of Aerospace Engineering

fig10

Figure 10

Figure 10: Numerical Investigation of an Axisymmetric Model Scramjet Assisted with Cavity of Different Aft Wall Angles 