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    Versatile Absolute Nodal Coordinate Formulation Model for Dynamic Folding Wing Deployment and Flutter Analyses 

    Source: Journal of Vibration and Acoustics:;2019:;volume( 141 ):;issue: 001:;page 11014
    Author(s): Otsuka, Keisuke; Wang, Yinan; Makihara, Kanjuro
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Aircraft performance can be improved using morphing wing technologies, in which the wing can be deployed and folded under flight conditions, providing a wide flight envelope, good fuel efficiency, and reducing the space ...
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    Absolute Nodal Coordinate Formulation With Vector-Strain Transformation for High Aspect Ratio Wings 

    Source: Journal of Computational and Nonlinear Dynamics:;2020:;volume( 016 ):;issue: 001:;page 011007-1
    Author(s): Otsuka, Keisuke; Wang, Yinan; Makihara, Kanjuro
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: High aspect ratio wings are potential candidates for use in atmospheric satellites and civil aircraft as they exhibit a low induced drag, which can reduce the fuel consumption. Owing to their slender and light weight ...
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    Recent Advances in the Absolute Nodal Coordinate Formulation: Literature Review From 2012 to 2020 

    Source: Journal of Computational and Nonlinear Dynamics:;2022:;volume( 017 ):;issue: 008:;page 80803-1
    Author(s): Otsuka, Keisuke; Makihara, Kanjuro; Sugiyama, Hiroyuki
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Absolute nodal coordinate formulation (ANCF) is a nonincremental nonlinear finite element procedure that has been successfully applied to the large deformation analysis of multibody systems for more than two decades. ...
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    Three-Dimensional Aeroelastic Model for Successive Analyses of High-Aspect-Ratio Wings 

    Source: Journal of Vibration and Acoustics:;2021:;volume( 143 ):;issue: 006:;page 061006-1
    Author(s): Otsuka, Keisuke; Wang, Yinan; Makihara, Kanjuro
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Next-generation civil aircraft and atmospheric satellites will have high-aspect-ratio wings. Such a design necessitates successive analysis of static, frequency, and time-domain dynamic responses based on a three-dimensional ...
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    Consistent Strain-Based Multifidelity Modeling for Geometrically Nonlinear Beam Structures 

    Source: Journal of Computational and Nonlinear Dynamics:;2022:;volume( 017 ):;issue: 011:;page 111003
    Author(s): Otsuka, Keisuke;Wang, Yinan;Fujita, Koji;Nagai, Hiroki;Makihara, Kanjuro
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Conventional multifidelity modeling for slender structures such as folding-wing aircraft and offshore wind turbines does not allow the generation of multiple fidelity models that consistently use the same external force ...
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    Nonlinear Dynamic Analysis Framework for Slender Structures Using the Modal Rotation Method 

    Source: Journal of Computational and Nonlinear Dynamics:;2024:;volume( 020 ):;issue: 002:;page 21002-1
    Author(s): Shizuno, Yoshitaka; Dong, Shuonan; Kuzuno, Ryo; Okada, Taiki; Kawashima, Shugo; Makihara, Kanjuro; Otsuka, Keisuke
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Owing to their low induced drag, high-aspect-ratio wings are often applied to aircraft, particularly high-altitude long-endurance (HALE) aircraft. An analytical method that considers geometrical nonlinearity is necessary ...
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