Modeling and Simulation of Solid Rocket Motors and Propellants

Chair:	Co-chair:
Wen Ao	Wenjing Yang
Northwestern Polytechnical University, China	Northwestern Polytechnical University, China

Summary:

The future solid rocket motor technology has a development trend of high energy, high pressure, and high intelligence, and combustion flow is the most critical process for propellant energy release. Accurate modeling, numerical simulation, and data-driven technology are challenges faced in improving the level of SRM design. This topic will focus on the digital frontier research of SRM, condense the common basic problems of modeling and simulation of SRM and propellants, propose key directions for refined simulation, and provide inspiration for the development of aerospace power technology.

Submission Deadline: 2025.6.1