Numerical study on flow-field characteristics and combustion stability of a rocket engine with a pintle injector

Acta Astronautica 2026

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Authors: Hao Zhang, Fan Zhao, Haibin Zhang, Bofeng Bai
DOI: 10.1016/j.actaastro.2026.03.051
Cited by: 1
References: 49

Fields of Study & Subjects

Rocket and propulsion systems research Computational Fluid Dynamics and Aerodynamics Combustion and flame dynamics

Publication details

Journal / source
Acta Astronautica
Publisher
Elsevier BV
Volume
246
Pages
276–292
Publication date
8 April 2026
Language
EN