Pages that link to "Item:Q1649726"
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The following pages link to Assessment of the LD-DSMC hybrid method for hypersonic rarefied flow (Q1649726):
Displaying 10 items.
- Hybrid continuum/DSMC computation of rocket mode lightcraft flow in near space with high temperature and rarefaction effect (Q435398) (← links)
- The effects of gurney flap on the aerodynamic performance of NACA 0012 airfoil in the rarefied gas flow (Q720902) (← links)
- A hybrid particle approach for continuum and rarefied flow simulation (Q1010327) (← links)
- Assessment of the cubic Fokker-Planck-DSMC hybrid method for hypersonic rarefied flows past a cylinder (Q1649829) (← links)
- A hybrid particle approach based on the unified stochastic particle Bhatnagar-Gross-Krook and DSMC methods (Q2123914) (← links)
- DSMC simulation of hypersonic flows using an improved SBT-TAS technique (Q2374846) (← links)
- Extension of the DSMC method to high pressure flows (Q3551620) (← links)
- Information preservation optimization method based on the advection upstream splitting method in supersonic rarefied flow simulation (Q6054212) (← links)
- Unified stochastic particle simulation of polyatomic gas flows using SPARTACUS (Q6095906) (← links)
- A second-order particle Fokker-Planck model for rarefied gas flows (Q6592781) (← links)