Research on Flow Characteristics of a Variable Mach Number Aerodynamic Test Device by a Rotating Profile by Zaicheng Chen, Yang Liu, Futing Bao, Ran Wei

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Precise Design of Solid Rocket Motor Heat Insulation Layer Thickness under Nonuniform Dynamic Burning Rate by Ran Wei, Futing Bao, Yang Liu, Weihua Hui

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Erratum to “Combined Acceleration Methods for Solid Rocket Motor Grain Burnback Simulation Based on the Level Set Method” by Ran Wei, Futing Bao, Yang Liu, Weihua Hui

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A New Erosive Burning Model of Solid Propellant Based on Heat Transfer Equilibrium at Propellant Surface by Yanjie Ma, Futing Bao, Lin Sun, Yang Liu, Weihua Hui

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Coupled Thermo-Structural Analysis Model of Solid Rocket Motor Nozzle considering the Variation of Friction Coefficient under Operating Conditions by Lin Sun, Huiyin Jia, Nan Zhang, Yu Zhao, Futing Bao

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Reverse design of solid propellant grain based on deep learning: Imaging internal ballistic data by Lin Sun, Xiangyu Peng, Yang Liu, Shu Long, Weihua Hui, Ran Wei, Futing Bao

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