Search alternatives:
greatest decrease » treatment decreased (Expand Search), greater increase (Expand Search)
increase decrease » increased release (Expand Search), increased crash (Expand Search)
linear decrease » linear increase (Expand Search)
greatest decrease » treatment decreased (Expand Search), greater increase (Expand Search)
increase decrease » increased release (Expand Search), increased crash (Expand Search)
linear decrease » linear increase (Expand Search)
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4961
Effects on cooling air mass flow rate.
Published 2025“…The results reveal that the large deviation in the manufactured vane (up to 0.5 mm at the leading edge) alters the direction of the coolant flowing out from the leading-edge film-cooling holes, affects the film coverage along the surface, and in consequence, causes the temperature near the stagnation point increasing by approximately 40 K. Furthermore, variations in coolant inlet pressure, decreasing by 10 kPa, and temperature, increasing by 10 K, result in the vane surface temperature increased by 20 ~ 30 K. …”
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4962
3D model and section view of E3 NGV.
Published 2025“…The results reveal that the large deviation in the manufactured vane (up to 0.5 mm at the leading edge) alters the direction of the coolant flowing out from the leading-edge film-cooling holes, affects the film coverage along the surface, and in consequence, causes the temperature near the stagnation point increasing by approximately 40 K. Furthermore, variations in coolant inlet pressure, decreasing by 10 kPa, and temperature, increasing by 10 K, result in the vane surface temperature increased by 20 ~ 30 K. …”
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4963
Conditions for uncertainty analyses.
Published 2025“…The results reveal that the large deviation in the manufactured vane (up to 0.5 mm at the leading edge) alters the direction of the coolant flowing out from the leading-edge film-cooling holes, affects the film coverage along the surface, and in consequence, causes the temperature near the stagnation point increasing by approximately 40 K. Furthermore, variations in coolant inlet pressure, decreasing by 10 kPa, and temperature, increasing by 10 K, result in the vane surface temperature increased by 20 ~ 30 K. …”
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4964
Scheme for mesh convergence study.
Published 2025“…The results reveal that the large deviation in the manufactured vane (up to 0.5 mm at the leading edge) alters the direction of the coolant flowing out from the leading-edge film-cooling holes, affects the film coverage along the surface, and in consequence, causes the temperature near the stagnation point increasing by approximately 40 K. Furthermore, variations in coolant inlet pressure, decreasing by 10 kPa, and temperature, increasing by 10 K, result in the vane surface temperature increased by 20 ~ 30 K. …”
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4965
Main test parameters.
Published 2025“…The results reveal that the large deviation in the manufactured vane (up to 0.5 mm at the leading edge) alters the direction of the coolant flowing out from the leading-edge film-cooling holes, affects the film coverage along the surface, and in consequence, causes the temperature near the stagnation point increasing by approximately 40 K. Furthermore, variations in coolant inlet pressure, decreasing by 10 kPa, and temperature, increasing by 10 K, result in the vane surface temperature increased by 20 ~ 30 K. …”
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4966
3-D printed NGV specimen.
Published 2025“…The results reveal that the large deviation in the manufactured vane (up to 0.5 mm at the leading edge) alters the direction of the coolant flowing out from the leading-edge film-cooling holes, affects the film coverage along the surface, and in consequence, causes the temperature near the stagnation point increasing by approximately 40 K. Furthermore, variations in coolant inlet pressure, decreasing by 10 kPa, and temperature, increasing by 10 K, result in the vane surface temperature increased by 20 ~ 30 K. …”
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4967
Relative error bar of surface temperature.
Published 2025“…The results reveal that the large deviation in the manufactured vane (up to 0.5 mm at the leading edge) alters the direction of the coolant flowing out from the leading-edge film-cooling holes, affects the film coverage along the surface, and in consequence, causes the temperature near the stagnation point increasing by approximately 40 K. Furthermore, variations in coolant inlet pressure, decreasing by 10 kPa, and temperature, increasing by 10 K, result in the vane surface temperature increased by 20 ~ 30 K. …”
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4968
Effect on the NGV leading edge temperature.
Published 2025“…The results reveal that the large deviation in the manufactured vane (up to 0.5 mm at the leading edge) alters the direction of the coolant flowing out from the leading-edge film-cooling holes, affects the film coverage along the surface, and in consequence, causes the temperature near the stagnation point increasing by approximately 40 K. Furthermore, variations in coolant inlet pressure, decreasing by 10 kPa, and temperature, increasing by 10 K, result in the vane surface temperature increased by 20 ~ 30 K. …”
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4969
Schematic of the test equipment.
Published 2025“…The results reveal that the large deviation in the manufactured vane (up to 0.5 mm at the leading edge) alters the direction of the coolant flowing out from the leading-edge film-cooling holes, affects the film coverage along the surface, and in consequence, causes the temperature near the stagnation point increasing by approximately 40 K. Furthermore, variations in coolant inlet pressure, decreasing by 10 kPa, and temperature, increasing by 10 K, result in the vane surface temperature increased by 20 ~ 30 K. …”
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4970
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4971
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4972
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4973
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4974
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4975
Results of SD-TOPSIS application ‐ combination A.
Published 2024“…Based on the performed analyses, we can see that significant differences result from their reduction. …”
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4976
ANOM analysis of evaluated criteria K1–K5.
Published 2024“…Based on the performed analyses, we can see that significant differences result from their reduction. …”
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4977
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4978
Effects of administering drugs into the TG on the glial fibrillary acidic protein (GFAP)-IR cells.
Published 2025“…N = 5 in each group. Significant increases were found in the ION-CCI, ION-CCI + vehi, ION-CCI + CGRP, and ION-CCI + ctrl IgG groups as compared to the sham group. …”
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4979
Experimental Analysis of Paraffin Deposition in Slug Flow
Published 2025“…However, increasing gas velocity further led to higher shear stress, which resulted in a reduction in wax buildup through shear stripping (∼62 g decrease). …”
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4980
Experimental Analysis of Paraffin Deposition in Slug Flow
Published 2025“…However, increasing gas velocity further led to higher shear stress, which resulted in a reduction in wax buildup through shear stripping (∼62 g decrease). …”