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A New Simulation Method for 3D Propellant Grain Burn Analysis of Solid Rocket Motor
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作者 方蜀州 胡克娴 张平 《Journal of Beijing Institute of Technology》 EI CAS 1995年第2期214+207-214,共9页
Describes a new computer program (Regress-3D) to simulate the regression of complex 3D grain cavity and calculate the burning surface area. It has a large region of applicability in solid rocket motor design and has... Describes a new computer program (Regress-3D) to simulate the regression of complex 3D grain cavity and calculate the burning surface area. It has a large region of applicability in solid rocket motor design and has made new improvements compared with other available codes. User can easily and rapidly build his initial grain shapes and then obtain geometric information of his design. Considering with the calclulting results, redesigning can be performed as desire until reaching at the satisfied result. Advantages and disadvantages of this method are also discussed. 展开更多
关键词 solid propellant rocket engines propellant grains computerized simulation COMBUSTION
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