Showing 4,481 - 4,500 results of 21,342 for search '(( significant degs decrease ) OR ( significant decrease decrease ))', query time: 0.42s Refine Results
  1. 4481

    Comparison with Existing Studies. by Na Zhao (112953)

    Published 2025
    “…The results indicate that: (1) the presence of pores prolongs both the time to failure and the onset of the AE burst stage, with longer durations observed at higher pore dip angles; (2) AE signal amplitude and frequency vary significantly across different loading stages, and the b-value exhibits an “increase–fluctuation–decrease” trend, with the decreasing stage serving as a precursor to rock instability; (3) pore dip angle strongly influences crack propagation types: dip angles of 0°–30° favor axial cracks and through-going wing cracks, 45°–75° angles tend to induce co-planar and wing crack connectivity, while 90° angles cause crack deviation, hindering through-going failure; (4) intact rock fails in a tensile–shear mixed mode, whereas the number of shear cracks in rocks with pores initially increases and then decreases with dip angle, reaching a maximum at 45°, resulting in shear-dominated failure. …”
  2. 4482

    Specimen Preparation and Experimental Setup. by Na Zhao (112953)

    Published 2025
    “…The results indicate that: (1) the presence of pores prolongs both the time to failure and the onset of the AE burst stage, with longer durations observed at higher pore dip angles; (2) AE signal amplitude and frequency vary significantly across different loading stages, and the b-value exhibits an “increase–fluctuation–decrease” trend, with the decreasing stage serving as a precursor to rock instability; (3) pore dip angle strongly influences crack propagation types: dip angles of 0°–30° favor axial cracks and through-going wing cracks, 45°–75° angles tend to induce co-planar and wing crack connectivity, while 90° angles cause crack deviation, hindering through-going failure; (4) intact rock fails in a tensile–shear mixed mode, whereas the number of shear cracks in rocks with pores initially increases and then decreases with dip angle, reaching a maximum at 45°, resulting in shear-dominated failure. …”
  3. 4483

    UCS texts data. by Na Zhao (112953)

    Published 2025
    “…The results indicate that: (1) the presence of pores prolongs both the time to failure and the onset of the AE burst stage, with longer durations observed at higher pore dip angles; (2) AE signal amplitude and frequency vary significantly across different loading stages, and the b-value exhibits an “increase–fluctuation–decrease” trend, with the decreasing stage serving as a precursor to rock instability; (3) pore dip angle strongly influences crack propagation types: dip angles of 0°–30° favor axial cracks and through-going wing cracks, 45°–75° angles tend to induce co-planar and wing crack connectivity, while 90° angles cause crack deviation, hindering through-going failure; (4) intact rock fails in a tensile–shear mixed mode, whereas the number of shear cracks in rocks with pores initially increases and then decreases with dip angle, reaching a maximum at 45°, resulting in shear-dominated failure. …”
  4. 4484

    S1 File - by Ingmar Lundquist (46422)

    Published 2025
    “…Additionally, the significance of extracellular NO on GSIS was studied. …”
  5. 4485
  6. 4486
  7. 4487
  8. 4488
  9. 4489
  10. 4490
  11. 4491

    Amplitude for A/L = 0.29. by Muhammad Hammad Bucha (21736111)

    Published 2025
    “…Increased surface roughness significantly reduced power output, flapping frequency, and amplitude. …”
  12. 4492

    Top view of the experimental setup. by Muhammad Hammad Bucha (21736111)

    Published 2025
    “…Increased surface roughness significantly reduced power output, flapping frequency, and amplitude. …”
  13. 4493

    Amplitude for A/L = 0.338. by Muhammad Hammad Bucha (21736111)

    Published 2025
    “…Increased surface roughness significantly reduced power output, flapping frequency, and amplitude. …”
  14. 4494

    Parameters of energy harvesting. by Muhammad Hammad Bucha (21736111)

    Published 2025
    “…Increased surface roughness significantly reduced power output, flapping frequency, and amplitude. …”
  15. 4495

    Graph for Max Amplitude/Length at G<sub>y</sub> = 0. by Muhammad Hammad Bucha (21736111)

    Published 2025
    “…Increased surface roughness significantly reduced power output, flapping frequency, and amplitude. …”
  16. 4496

    Amplitude for A/L = 0.02. by Muhammad Hammad Bucha (21736111)

    Published 2025
    “…Increased surface roughness significantly reduced power output, flapping frequency, and amplitude. …”
  17. 4497

    Graph for maximum Frequency at G<sub>y</sub> = 0. by Muhammad Hammad Bucha (21736111)

    Published 2025
    “…Increased surface roughness significantly reduced power output, flapping frequency, and amplitude. …”
  18. 4498

    Graph for maximum Power at G<sub>y</sub> = 0. by Muhammad Hammad Bucha (21736111)

    Published 2025
    “…Increased surface roughness significantly reduced power output, flapping frequency, and amplitude. …”
  19. 4499

    Amplitude for A/L = 0.03. by Muhammad Hammad Bucha (21736111)

    Published 2025
    “…Increased surface roughness significantly reduced power output, flapping frequency, and amplitude. …”
  20. 4500

    Summary of experimentation results. by Muhammad Hammad Bucha (21736111)

    Published 2025
    “…Increased surface roughness significantly reduced power output, flapping frequency, and amplitude. …”