Showing 4,961 - 4,980 results of 13,227 for search '(( significantly ((linear decrease) OR (greatest decrease)) ) OR ( significant increase decrease ))', query time: 0.53s Refine Results
  1. 4961

    Effects on cooling air mass flow rate. by Decang Lou (21439960)

    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. …”
  2. 4962

    3D model and section view of E3 NGV. by Decang Lou (21439960)

    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. …”
  3. 4963

    Conditions for uncertainty analyses. by Decang Lou (21439960)

    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. …”
  4. 4964

    Scheme for mesh convergence study. by Decang Lou (21439960)

    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. …”
  5. 4965

    Main test parameters. by Decang Lou (21439960)

    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. …”
  6. 4966

    3-D printed NGV specimen. by Decang Lou (21439960)

    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. …”
  7. 4967

    Relative error bar of surface temperature. by Decang Lou (21439960)

    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. …”
  8. 4968

    Effect on the NGV leading edge temperature. by Decang Lou (21439960)

    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. …”
  9. 4969

    Schematic of the test equipment. by Decang Lou (21439960)

    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. …”
  10. 4970
  11. 4971
  12. 4972
  13. 4973
  14. 4974
  15. 4975

    Results of SD-TOPSIS application ‐ combination A. by Roman Vavrek (13200141)

    Published 2024
    “…Based on the performed analyses, we can see that significant differences result from their reduction. …”
  16. 4976

    ANOM analysis of evaluated criteria K1–K5. by Roman Vavrek (13200141)

    Published 2024
    “…Based on the performed analyses, we can see that significant differences result from their reduction. …”
  17. 4977
  18. 4978

    Effects of administering drugs into the TG on the glial fibrillary acidic protein (GFAP)-IR cells. by Hiroharu Maegawa (8087543)

    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. …”
  19. 4979

    Experimental Analysis of Paraffin Deposition in Slug Flow by Aziz Alhejaili (10331604)

    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). …”
  20. 4980

    Experimental Analysis of Paraffin Deposition in Slug Flow by Aziz Alhejaili (10331604)

    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). …”