International Journal of Aerospace Engineering / 2020 / Article / Tab 1

Research Article

Numerical Study of Disturbance Resistance of Oblique Detonation Waves

Table 1

Numerical parameter setup.

Inflow Mach number, Inflow static temperature, (K)Inflow static pressure, (pa)Specific heat ratio, Dimensionless heat release,

4.0650200001.28
Dimensionless activation energy of the induction step, Dimensionless activation energy of the heat release step, Induction length corresponding to a CJ detonation, (mm)Thermal pulse width corresponding to a CJ detonation, (mm)Gas constant, (J/kg·K)
4.81.02.120.95377.9