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Showing 1 - 4 results of 4 for search '(bills OR (fill OR half)) ((drago OR drag) OR (dragos OR ragon))', query time: 0.19s Refine Results
  1. 1
    Development of a multi-rotor VTOL UAV : numerical study of rotor-wake induced interference drag on a VTOL UAV

    Development of a multi-rotor VTOL UAV : numerical study of rotor-wake induced interference drag on a VTOL UAV by Lim, Jarad Jian An

    Published 2018
    “…Methods for determining the inputs to these MA models are validated, and the MA model is used on a half-body Electric Vertical Take-Off and Landing (eVTOL) aircraft. …”
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    Final Year Project (FYP)
  2. 2
    Active control of wakes and vortex-induced vibration of a circular cylinder at Re = 100

    Active control of wakes and vortex-induced vibration of a circular cylinder at Re = 100 by Wang, Chenglei

    Published 2016
    “…As zero net-mass-flux jets, SJs have been widely applied in flow separation control and drag reduction for bluff bodies. However, their implementation for VIV control is rare and still remains not fully understood. …”
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    Thesis
  3. 3
    An experimental and simulation study of chip transportation behaviour in gundrilling

    An experimental and simulation study of chip transportation behaviour in gundrilling by Tnay, Guan Leong

    Published 2017
    “…From the experiments, terminal velocities of typical gun drill chips at different range of particle Reynolds number were determined to construct the unique drag curve. Based on the findings, a computational fluid dynamic (CFD) numerical model was developed to predict the lateral drag forces with respect to the particle Reynolds number. …”
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    Thesis
  4. 4
    Determination of operating point for a propulsive wing UAV using CFD

    Determination of operating point for a propulsive wing UAV using CFD by Chan, Chee Shuan

    Published 2018
    “…CFD simulations were performed using a 2D RANS k-ε turbulence model and the rotating flow was captured using the moving reference frame method. Lift and drag were obtained for different angle of attacks via a control volume analysis of CFD results. …”
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    Final Year Project (FYP)

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