Showing 13,981 - 14,000 results of 61,004 for search '(( a ((((laser decrease) OR (mean decrease))) OR (linear decrease)) ) OR ( a large decrease ))', query time: 1.30s Refine Results
  1. 13981

    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. …”
  2. 13982

    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. …”
  3. 13983

    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. …”
  4. 13984

    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. …”
  5. 13985

    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. …”
  6. 13986

    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. …”
  7. 13987

    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. …”
  8. 13988

    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. …”
  9. 13989

    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. …”
  10. 13990

    Fig 3 - 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. …”
  11. 13991

    Fig 1 - 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. 13992

    Fig 6 - 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. 13993

    Simvastatin reduces vinculin localization at cell-cell adhesions in endothelial monolayers. by Marsha C. Lampi (845609)

    Published 2016
    “…(C) Vinculin localization per monolayer at cell-cell adhesions, a readout of intercellular junction tension, is quantified and increases with matrix stiffness but is significantly decreased with the statin treatment at higher matrix stiffnesses (n = 3, 70–90 fields of view per condition). …”
  14. 13994

    Effect of BM pretreatment on CYP3A at mRNA and functional activity level. by Rajbir Singh (451210)

    Published 2013
    “…BM treatment decreases the mRNA levels of CYP3A1and CYP3A2 in liver and intestine as assessed by real-time PCR as described in Materials and Methods. …”
  15. 13995
  16. 13996
  17. 13997

    Efficacy and safety of a single radiofrequency ablation of solid benign non-functioning thyroid nodules by Roberto Cesareo (4676131)

    Published 2018
    “…Forty-eight patients with solid, non-functioning BTNs were treated by RFA using a 17G internally cooled electrode. We categorized thyroid nodules as small (≤ 12 mL), medium (12 to 30 mL), or large (over 30 mL). …”
  18. 13998
  19. 13999
  20. 14000