Search Results - "Kwon, Kijung"

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  1. 1
    Effect of differential spoiler settings (DSS) on the wake vortices of a wing at high-lift-configuration (HLC)

    Effect of differential spoiler settings (DSS) on the wake vortices of a wing at high-lift-configuration (HLC) by Elsayed, Omer A., Omar, Ashraf A., Asrar, Waqar, Kwon, Kijung

    Published in Aerospace science and technology (01-10-2011)
    “…An experimental investigation has been carried out to evaluate the capabilities of differential spoiler setting (DSS) in modifying the wingspan loading. The…”
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  2. 2
    MEASUREMENTS OF PRESSURE DISTRIBUTIONS ON A ROTOR BLADE USING PSP TECHNIQUES

    MEASUREMENTS OF PRESSURE DISTRIBUTIONS ON A ROTOR BLADE USING PSP TECHNIQUES by Kim, Kidong, Kwon, Kijung

    Published in IIUM engineering journal (20-12-2011)
    “…Surface pressure distributions on a rotating blade were measured by using pressure sensitive paint (PSP) to understand aerodynamic characteristics of a rotor…”
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  3. 3
    Control of shear perturbation in coaxial swirling turbulent jets

    Control of shear perturbation in coaxial swirling turbulent jets by Lee, Wonjoong, Park, Youngmin, Kwon, Kijung, Taghavi, Ray

    Published in Aerospace science and technology (01-10-2010)
    “…The present study explores the swirl jet characteristics and the possibility of using artificial means for control of shear layers with the application as…”
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  4. 4
    Acoustic streaming pattern induced by longitudinal ultrasonic vibration in an open channel using particle imaging velocimetry

    Acoustic streaming pattern induced by longitudinal ultrasonic vibration in an open channel using particle imaging velocimetry by Loh, Byoung-Gook, Lee, Dong-Ryul, Kwon, Kijung

    Published in Applied physics letters (30-10-2006)
    “…Acoustic streaming, which is induced in an open channel by a cylindrical exciter vibrating at 30kHz, is experimentally investigated using particle imaging…”
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  5. 5
    Evolution of NACA23012 Wake Vortices Structure Using PIV

    Evolution of NACA23012 Wake Vortices Structure Using PIV by Elsayed, Omer A, Asrar, Waqar, Omar, Ashraf A, Kwon, Kijung

    Published in Journal of aerospace engineering (01-01-2012)
    “…The formation and development of a wing-tip vortex in a near and extended near field were studied experimentally. A swept-back tapered wing with a NACA23012…”
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  6. 6
    Acoustic streaming pattern induced by longitudinal ultrasonic vibrationin an open channel using particle imaging velocimetry

    Acoustic streaming pattern induced by longitudinal ultrasonic vibrationin an open channel using particle imaging velocimetry by Loh, Byoung-Gook, Lee, Dong-Ryul, Kwon, Kijung

    Published in Applied physics letters (31-10-2006)
    “…Acoustic streaming, which is induced in an open channel by a cylindrical exciter vibrating at 30 kHz , is experimentally investigated using particle imaging…”
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