Showing 13,441 - 13,460 results of 60,026 for search '(( a ((((teer decrease) OR (mean decrease))) OR (linear decrease)) ) OR ( a large decrease ))', query time: 0.66s Refine Results
  1. 13441
  2. 13442

    Cytotoxic effect of Eltrombopag on AML cells is dependent on dose and serum concentration. by Anna Kalota (7415)

    Published 2015
    “…Data are presented as an average of 3 independent experiments with a standard error of the mean (SEM). B) Time course of the response to 5 μM E in representative primary AML sample and MOLM14 cell line in 2% serum. …”
  3. 13443
  4. 13444
  5. 13445
  6. 13446

    Increased endothelial cell-cell junction size on stiff matrices is diminished after simvastatin treatment. by Marsha C. Lampi (845609)

    Published 2016
    “…Data are presented as means ± standard error of the mean,*p<0.05.</p>…”
  7. 13447
  8. 13448
  9. 13449

    A predictive strategy for lifetime maximization in selective relay networks by Mousavifar, S.A.

    Published 2009
    “…In this case, when the number of relays is large, the improvement is substantial. As the number of relays decreases, the method improves the lifetime under the condition of high initial energy levels at the relays. …”
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  10. 13450

    Ba<sub>2</sub>NaClP<sub>2</sub>O<sub>7</sub>: Unprecedented Phase Matchability Induced by Symmetry Breaking and Its Unique Fresnoite-Type Structure by Jie Chen (5892)

    Published 2018
    “…To combine noncentrosymmetry, large second order nonlinear optical (NLO) susceptibility, deep UV transparency, and phase matchability simultaneously into a single structure is a great challenge. …”
  11. 13451

    Fig 9 - by Qian Du (280345)

    Published 2024
    “…The aircraft with high aspect ratio wings is simplified as a hub-beam system. Such a rigid-flexible system with the fast rotation speed of hub and the large deformation of the beam is modeled using absolute coordinate-based formulation accurately. …”
  12. 13452

    Fig 10 - by Qian Du (280345)

    Published 2024
    “…The aircraft with high aspect ratio wings is simplified as a hub-beam system. Such a rigid-flexible system with the fast rotation speed of hub and the large deformation of the beam is modeled using absolute coordinate-based formulation accurately. …”
  13. 13453

    Fig 8 - by Qian Du (280345)

    Published 2024
    “…The aircraft with high aspect ratio wings is simplified as a hub-beam system. Such a rigid-flexible system with the fast rotation speed of hub and the large deformation of the beam is modeled using absolute coordinate-based formulation accurately. …”
  14. 13454

    Fig 12 - by Qian Du (280345)

    Published 2024
    “…The aircraft with high aspect ratio wings is simplified as a hub-beam system. Such a rigid-flexible system with the fast rotation speed of hub and the large deformation of the beam is modeled using absolute coordinate-based formulation accurately. …”
  15. 13455

    MATLAB program for numerical analysis. by Qian Du (280345)

    Published 2024
    “…The aircraft with high aspect ratio wings is simplified as a hub-beam system. Such a rigid-flexible system with the fast rotation speed of hub and the large deformation of the beam is modeled using absolute coordinate-based formulation accurately. …”
  16. 13456

    Fig 5 - by Qian Du (280345)

    Published 2024
    “…The aircraft with high aspect ratio wings is simplified as a hub-beam system. Such a rigid-flexible system with the fast rotation speed of hub and the large deformation of the beam is modeled using absolute coordinate-based formulation accurately. …”
  17. 13457

    Fig 2 - by Qian Du (280345)

    Published 2024
    “…The aircraft with high aspect ratio wings is simplified as a hub-beam system. Such a rigid-flexible system with the fast rotation speed of hub and the large deformation of the beam is modeled using absolute coordinate-based formulation accurately. …”
  18. 13458

    Fig 7 - by Qian Du (280345)

    Published 2024
    “…The aircraft with high aspect ratio wings is simplified as a hub-beam system. Such a rigid-flexible system with the fast rotation speed of hub and the large deformation of the beam is modeled using absolute coordinate-based formulation accurately. …”
  19. 13459

    Fig 4 - by Qian Du (280345)

    Published 2024
    “…The aircraft with high aspect ratio wings is simplified as a hub-beam system. Such a rigid-flexible system with the fast rotation speed of hub and the large deformation of the beam is modeled using absolute coordinate-based formulation accurately. …”
  20. 13460

    Fig 11 - by Qian Du (280345)

    Published 2024
    “…The aircraft with high aspect ratio wings is simplified as a hub-beam system. Such a rigid-flexible system with the fast rotation speed of hub and the large deformation of the beam is modeled using absolute coordinate-based formulation accurately. …”