AP/HTPB combustion response simulation with a new equivalent linear system method

Engineering

• Computational Fluid Dynamics 100%
• Burning Rate 60%
• Transfer Function 60%
• Relative Error 40%
• Simulation Result 20%
• Applicability 20%
• Rocket Engine 20%
• Black Box 20%
• Response Function 20%
• Pressure Perturbation 20%
• Simulated System 20%
• Burning Surface 20%
• Negative Pressure 20%
• Positive Pressure 20%
• Solid Modeling 20%
• Transient Combustion 20%