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Regression rate and combustion performance investigation on hybrid rocket motor with head-end swirl injection under high geometric swirl number

Guobiao Cai, Zeng Zhao, Bo Zhao, Yufei Liu, Nanjia Yu

2020Aerospace Science and Technology41 citationsDOI

Topics & Concepts

CombustionRocket (weapon)Head (geology)Fuel injectionMechanicsInjectorCombustion chamberMaterials scienceSolid-fuel rocketMass fluxMass flow rateTurbulenceAutomotive engineeringAerospace engineeringSimulationMechanical engineeringEngineeringPhysicsPropellantChemistryGeologyOrganic chemistryGeomorphologyRocket and propulsion systems researchEnergetic Materials and CombustionHeat transfer and supercritical fluids
Regression rate and combustion performance investigation on hybrid rocket motor with head-end swirl injection under high geometric swirl number | Litcius