Iterative calculations for solid rocket ramjet performances on design condition

Engineering

• Afterburner 50%
• Air Inlet 50%
• Data Table 50%
• Design Condition 100%
• Design Point 50%
• Iterative Algorithm 100%
• NASA 50%
• Performance Analysis 50%
• Pressure Recovery Coefficient 50%
• Scheme Design 50%
• Thermodynamic Calculation 50%
• Thermodynamic Parameter 50%