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    Influence of Geometric Coupling on the Whirl Flutter Stability in Tiltrotor Aircraft with Unsteady Aerodynamics 

    Source: Journal of Aerospace Engineering:;2012:;Volume ( 025 ):;issue: 001
    Author(s): Taeseong Kim; SangJoon Shin; Do-Hyung Kim
    Publisher: American Society of Civil Engineers
    Abstract: A further improvement is attempted of an existing analytical model for an accurate prediction of the aeroelastic stability of a tiltrotor aircraft. A rigid-bladed rotor structural model with the natural frequencies selected ...
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    Improved Aerodynamic Analysis for Multirotor-Type UAS Flight Simulation Using Dynamic Inflow and Rigid Blade Flapping 

    Source: Journal of Aerospace Engineering:;2020:;Volume ( 033 ):;issue: 004
    Author(s): SunHoo Park; JeongUk Yoo; SangJoon Shin
    Publisher: ASCE
    Abstract: Recently, studies on the control and aerodynamics of multirotor unmanned aircraft system (UAS) have been performed. However, some studies depend on methods that require significant computing time or are not applicable in ...
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    Computational Study of Fluid-Structure Interaction on Flapping Wing under Passive Pitching Motion 

    Source: Journal of Aerospace Engineering:;2019:;Volume ( 032 ):;issue: 004
    Author(s): Haeseong Cho; SangJoon Shin; Namhun Lee; Seungsoo Lee
    Publisher: American Society of Civil Engineers
    Abstract: During the past few decades, various fluid–structure interaction (FSI) analysis approaches have been developed and applied to understand the physical processes related to a flexible flapping wing. In this paper, a dynamic ...
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    Computational Study of Fluid-Structure Interaction on Flapping Wing under Passive Pitching Motion 

    Source: Journal of Aerospace Engineering:;2019:;Volume (032):;issue:004
    Author(s): Haeseong Cho;SangJoon Shin;Namhun Lee;Seungsoo Lee
    Publisher: American Society of Civil Engineers
    Abstract: During the past few decades, various fluid–structure interaction (FSI) analysis approaches have been developed and applied to understand the physical processes related to a flexible flapping wing. In this paper, a dynamic ...
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