Study of shock-shock interactions in rarefied flows using direct simulation Monte Carlo method
Authors:
- Yazhong JiangYJYazhong Jiang
- Xuxu SunXuxu Sun
- Jie NiuJNJie Niu
- Jun ZhangJZJun Zhang
- 30 January 2026
- journal article
- Published by Elsevier in Aerospace Science and Technology
- Vol. 173
Abstract
No abstract availableAll Related Versions
Funding Information
- Fundamental Research Funds for the Central Universities (104972024KFYjc0003)
- National Natural Science Foundation of China (12302388)
- National Natural Science Foundation of China (12302443)
This publication has 50 references indexed in Scilit:
- Drag and overall aeroheating reduction of a dual-disk-dual-jet in rarefied hypersonic flow in near spaceAerospace Science and Technology, 2025
- Thermo-chemical non-equilibrium flows and aerodynamic loads of Type III shock/shock interaction on blunted lip of a Mach 12 inletAerospace Science and Technology, 2025
- Experimental study on the detonation propagation behavior in a thin cylindrical chamberAerospace Science and Technology, 2025
- Numerical investigation on flow and aerothermal characteristics of rarefied hypersonic flows over slender cavitiesAerospace Science and Technology, 2023
- Study of a non-reacting hypersonic flow over an external cavity with flow injection using DSMC methodAerospace Science and Technology, 2023
- Aerodynamic drag analysis and reduction strategy for satellites in Very Low Earth OrbitAerospace Science and Technology, 2022
- The effect of increasing rarefaction on the formation of Edney shock interaction patterns: type-I to type-VIShock Waves, 2022
- Shock/shock interferences in a supersonic rarefied flow: experimental investigationExperiments in Fluids, 2021
- Characteristics of unsteady type IV shock/shock interactionShock Waves, 2012
- Statistical collision model for Monte Carlo simulation of polyatomic gas mixtureJournal of Computational Physics, 1975