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- W4386411909 abstract "The CFD simulation of aircraft cockpit flow field and temperature field is essentially a process of solving complex differential/integral equation (NS equation) based on the fixed solution conditions in a certain solution domain. The industry generally selects mature solvers integrated in software for CFD simulation, so it is necessary to know the influence of the solver settings on the calculation results, so as to form a recommended calculation execution scheme for the use of design and analysis personnel. This paper evaluates the sensitivity of different solver settings (model type, Prandtl number, turbulent viscosity ratio and turbulence intensity) to CFD simulation of cockpit, and gives a grading of their effects. The result shows that SST k-ω model should be cautiously selection, and model type and Prandtl number settings should receive more attention when cockpit simulating." @default.
- W4386411909 created "2023-09-05" @default.
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- W4386411909 date "2023-01-01" @default.
- W4386411909 modified "2023-10-16" @default.
- W4386411909 title "Sensitivity Analysis of Solver Setting for Cockpit CFD Calculation" @default.
- W4386411909 cites W2071054164 @default.
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- W4386411909 doi "https://doi.org/10.1007/978-981-99-4882-6_27" @default.
- W4386411909 hasPublicationYear "2023" @default.
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