On shock evolution and thrust variation of a rocket permeable nozzle in an ascent-descent operation

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Authors: Yuqin Xue, Ge Wang, Ben GUAN, Yuqi Jin, Lei Chen (54296)
Cited by: 1
References: 23

Fields of Study & Subjects

Computational Fluid Dynamics and Aerodynamics Gas Dynamics and Kinetic Theory Rocket and propulsion systems research

Publication details

Journal / source
Acta Mechanica Sinica
Publisher
Springer Science and Business Media LLC
Volume
42
Issue
3
Publication date
1 March 2026
Language
EN