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    Impact of Gurney Flaplike Strips on the Aerodynamic and Vortex Flow Characteristic of a Reverse Delta Wing 

    Source: Journal of Fluids Engineering:;2016:;volume( 138 ):;issue: 006:;page 61104
    Author(s): Lee, T.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The impact of Gurney flaplike strips, of different geometric configurations and heights, on the aerodynamic characteristics and the tip vortices generated by a reverse delta wing (RDW) was investigated via forcebalance ...
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    Wingtip Vortex Control Via Tip Mounted Half Delta Wings of Different Geometric Configurations 

    Source: Journal of Fluids Engineering:;2015:;volume( 137 ):;issue: 012:;page 121105
    Author(s): Lee, T.; Choi, S.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The control of the tip vortex, generated by a rectangular NACA 0012 wing, via tipmounted halfdelta wings (HDWs), of different slendernesses خ›, root chords cr, and deflections خ´, was investigated experimentally at ...
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    Effect of Ground Boundary Condition on Near-Field Wingtip Vortex Flow and Lift-Induced Drag 

    Source: Journal of Fluids Engineering:;2020:;volume( 143 ):;issue: 003:;page 031301-1
    Author(s): Lu, A.; Lee, T.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The ground proximity is known to induce an outboard movement and suppression of the wingtip vortices, leading to a reduced lift-induced drag. Depending on the ground boundary condition, a large scatter exists in the published ...
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    Surface Pressures Developed on an Airfoil Undergoing Heaving and Pitching Motion 

    Source: Journal of Fluids Engineering:;2015:;volume( 137 ):;issue: 005:;page 51105
    Author(s): Lee, T.; Su, Y. Y.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The surface pressure distributions and flow patterns developed on and around a NACA 0012 airfoil undergoing heaving and pitching were investigated at Re = 3.6 أ— 104. Despite extensive investigations conducted by ...
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    Aerodynamics and Vortex Flowfield of a Slender Delta Wing With Apex Flap and Tip Flap 

    Source: Journal of Fluids Engineering:;2017:;volume( 139 ):;issue: 005:;page 51106
    Author(s): Lee, T.; Ko, L. S.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The effect of apex flap and tip flap, deflected both independently and jointly, on the vortex flow and lift generation of a 65 deg-sweep delta wing was investigated experimentally. The drooped apex flap produced a higher ...
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    Experimental Investigation of the Aerodynamics and Flowfield of a NACA 0015 Airfoil Over a Wavy Ground 

    Source: Journal of Fluids Engineering:;2018:;volume( 140 ):;issue: 007:;page 71202
    Author(s): Lee, T.; Tremblay-Dionne, V.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Experimental Investigation of the Aerodynamics and Flowfield of a NACA 0015 Airfoil Over a Wavy Ground;The aerodynamic properties and flowfield of a NACA 0015 airfoil over a wavy ground were investigated experimentally via ...
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    Ground Effect on the Vortex Flow and Aerodynamics of a Slender Delta Wing 

    Source: Journal of Fluids Engineering:;2018:;volume( 140 ):;issue: 007:;page 71104
    Author(s): Lee, T.; Ko, L. S.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The ground effect on the aerodynamic loading and leading-edge vortex (LEV) flow generated by a slender delta wing was investigated experimentally. Both the lift and drag forces were found to increase with reducing ground ...
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    Effect of Trailing-Edge Flap Deflection on a Symmetric Airfoil Over a Wavy Ground 

    Source: Journal of Fluids Engineering:;2019:;volume( 141 ):;issue: 006:;page 64501
    Author(s): Tremblay-Dionne, V.; Lee, T.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The effect of trailing-edge flap (TEF) deflection on the aerodynamic properties and flowfield of a symmetric airfoil over a wavy ground was investigated experimentally. This Technical Brief is a continuation of Lee and ...
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    Heat Transfer of a Rotating Rectangular Channel With a Diamond Shaped Pin Fin Array at High Rotation Numbers 

    Source: Journal of Turbomachinery:;2013:;volume( 135 ):;issue: 004:;page 41007
    Author(s): Chang, S. W.; Liou, T.; Lee, T.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This experimental study measured the detailed Nusselt numbers (Nu) distributions over two opposite leading and trailing walls of a rotating rectangular channel fitted with a diamondshaped pinfin array with radially outward ...
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    Experimental Study of Aerodynamics and Wingtip Vortex of a Rectangular Wing in Flat Ground Effect 

    Source: Journal of Fluids Engineering:;2019:;volume( 141 ):;issue: 011:;page 111108
    Author(s): Lu, A.; Tremblay-Dionne, V.; Lee, T.
    Publisher: American Society of Mechanical Engineers (ASME)
    Abstract: The ground effect on the aerodynamics and tip vortex flow of a rectangular wing is investigated experimentally at Re = 2.71 × 105. The results show that there is a large lift increase with reducing ground distance. By ...
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