Numerical analysis of the hybrid rocket motor with axial injection based on oxidizer flow distribution
Hui Tian, Xianzhu Jiang, Ruipeng Yu, Hao Zhu, Yuanjun Zhang, Guobiao Cai
Topics & Concepts
MechanicsInjectorSolid-fuel rocketMass flow rateMaterials scienceCombustionCombustion chamberPropellantFuel injectionRocket (weapon)Flow (mathematics)Mass flowAerospace engineeringMechanical engineeringChemistryPhysicsEngineeringOrganic chemistryRocket and propulsion systems researchEnergetic Materials and CombustionAerospace Engineering and Control Systems