Search alternatives:
significant decrease » significant increase (Expand Search), significantly increased (Expand Search)
point decrease » point increase (Expand Search)
main decrease » gain decreased (Expand Search), mean decrease (Expand Search), small decrease (Expand Search)
significant decrease » significant increase (Expand Search), significantly increased (Expand Search)
point decrease » point increase (Expand Search)
main decrease » gain decreased (Expand Search), mean decrease (Expand Search), small decrease (Expand Search)
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62
Scheme of the test section.
Published 2025“…Computational fluid dynamic analysis indicates that the shear stress transport turbulence model gives high accuracy in simulating the vane main-stream aerodynamic performance. However, when the simulated surface temperature of the vane was compared with the cooling test data, in which the vane was 3D-printed, significant deviation of the surface temperature distribution was observed. …”
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63
Effects on cooling air mass flow rate.
Published 2025“…Computational fluid dynamic analysis indicates that the shear stress transport turbulence model gives high accuracy in simulating the vane main-stream aerodynamic performance. However, when the simulated surface temperature of the vane was compared with the cooling test data, in which the vane was 3D-printed, significant deviation of the surface temperature distribution was observed. …”
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64
3D model and section view of E3 NGV.
Published 2025“…Computational fluid dynamic analysis indicates that the shear stress transport turbulence model gives high accuracy in simulating the vane main-stream aerodynamic performance. However, when the simulated surface temperature of the vane was compared with the cooling test data, in which the vane was 3D-printed, significant deviation of the surface temperature distribution was observed. …”
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65
Conditions for uncertainty analyses.
Published 2025“…Computational fluid dynamic analysis indicates that the shear stress transport turbulence model gives high accuracy in simulating the vane main-stream aerodynamic performance. However, when the simulated surface temperature of the vane was compared with the cooling test data, in which the vane was 3D-printed, significant deviation of the surface temperature distribution was observed. …”
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66
Scheme for mesh convergence study.
Published 2025“…Computational fluid dynamic analysis indicates that the shear stress transport turbulence model gives high accuracy in simulating the vane main-stream aerodynamic performance. However, when the simulated surface temperature of the vane was compared with the cooling test data, in which the vane was 3D-printed, significant deviation of the surface temperature distribution was observed. …”
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67
3-D printed NGV specimen.
Published 2025“…Computational fluid dynamic analysis indicates that the shear stress transport turbulence model gives high accuracy in simulating the vane main-stream aerodynamic performance. However, when the simulated surface temperature of the vane was compared with the cooling test data, in which the vane was 3D-printed, significant deviation of the surface temperature distribution was observed. …”
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68
Relative error bar of surface temperature.
Published 2025“…Computational fluid dynamic analysis indicates that the shear stress transport turbulence model gives high accuracy in simulating the vane main-stream aerodynamic performance. However, when the simulated surface temperature of the vane was compared with the cooling test data, in which the vane was 3D-printed, significant deviation of the surface temperature distribution was observed. …”
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69
Effect on the NGV leading edge temperature.
Published 2025“…Computational fluid dynamic analysis indicates that the shear stress transport turbulence model gives high accuracy in simulating the vane main-stream aerodynamic performance. However, when the simulated surface temperature of the vane was compared with the cooling test data, in which the vane was 3D-printed, significant deviation of the surface temperature distribution was observed. …”
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70
Schematic of the test equipment.
Published 2025“…Computational fluid dynamic analysis indicates that the shear stress transport turbulence model gives high accuracy in simulating the vane main-stream aerodynamic performance. However, when the simulated surface temperature of the vane was compared with the cooling test data, in which the vane was 3D-printed, significant deviation of the surface temperature distribution was observed. …”
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71
Effect of the Surface Peak–Valley Features on Droplet Impact Dynamics under Leidenfrost Temperature
Published 2024“…Specifically, the Leidenfrost temperature on micropit surfaces increases with greater micropit area occupancy, while it decreases on micropillar surfaces under similar conditions, which is mainly attributed to the differential impact of area occupancy on droplet heat transfer efficiency. …”
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72
Effect of the Surface Peak–Valley Features on Droplet Impact Dynamics under Leidenfrost Temperature
Published 2024“…Specifically, the Leidenfrost temperature on micropit surfaces increases with greater micropit area occupancy, while it decreases on micropillar surfaces under similar conditions, which is mainly attributed to the differential impact of area occupancy on droplet heat transfer efficiency. …”
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73
Effect of the Surface Peak–Valley Features on Droplet Impact Dynamics under Leidenfrost Temperature
Published 2024“…Specifically, the Leidenfrost temperature on micropit surfaces increases with greater micropit area occupancy, while it decreases on micropillar surfaces under similar conditions, which is mainly attributed to the differential impact of area occupancy on droplet heat transfer efficiency. …”
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74
Effect of the Surface Peak–Valley Features on Droplet Impact Dynamics under Leidenfrost Temperature
Published 2024“…Specifically, the Leidenfrost temperature on micropit surfaces increases with greater micropit area occupancy, while it decreases on micropillar surfaces under similar conditions, which is mainly attributed to the differential impact of area occupancy on droplet heat transfer efficiency. …”
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75
Effect of the Surface Peak–Valley Features on Droplet Impact Dynamics under Leidenfrost Temperature
Published 2024“…Specifically, the Leidenfrost temperature on micropit surfaces increases with greater micropit area occupancy, while it decreases on micropillar surfaces under similar conditions, which is mainly attributed to the differential impact of area occupancy on droplet heat transfer efficiency. …”
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76
Effect of the Surface Peak–Valley Features on Droplet Impact Dynamics under Leidenfrost Temperature
Published 2024“…Specifically, the Leidenfrost temperature on micropit surfaces increases with greater micropit area occupancy, while it decreases on micropillar surfaces under similar conditions, which is mainly attributed to the differential impact of area occupancy on droplet heat transfer efficiency. …”
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77
Effect of the Surface Peak–Valley Features on Droplet Impact Dynamics under Leidenfrost Temperature
Published 2024“…Specifically, the Leidenfrost temperature on micropit surfaces increases with greater micropit area occupancy, while it decreases on micropillar surfaces under similar conditions, which is mainly attributed to the differential impact of area occupancy on droplet heat transfer efficiency. …”
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78
Effect of the Surface Peak–Valley Features on Droplet Impact Dynamics under Leidenfrost Temperature
Published 2024“…Specifically, the Leidenfrost temperature on micropit surfaces increases with greater micropit area occupancy, while it decreases on micropillar surfaces under similar conditions, which is mainly attributed to the differential impact of area occupancy on droplet heat transfer efficiency. …”
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79
A schematic view of ACS.
Published 2025“…The effect of concentration solution, primary heat exchanger effectiveness, and the temperature of main component (generator, condenser, evaporator and absorber) are studied. …”
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80
Assumed conditions.
Published 2025“…The effect of concentration solution, primary heat exchanger effectiveness, and the temperature of main component (generator, condenser, evaporator and absorber) are studied. …”