Search Results - 한국항공우주학회

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  1. 1

    Impact and Delamination Failure of Multiscale Carbon Nanotube-Fiber Reinforced Polymer Composites: A Review by Khan, Shafi Ullah, Kim, Jang-Kyo

    ISSN: 2093-274X, 2093-2480
    Published: 한국항공우주학회 30.06.2011
    “…Fiber reinforced polymer composites (FRPs) are being increasingly used for a wide range of engineering applications owing to their high specific strength and…”
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    Journal Article
  2. 2

    A Development and Assessment of Variable-Incidence Angle Vortex Generator at Low Reynolds Number of ~ 5×10^4 by Ho-Hyun Kim, Ho-Young Kim, Jong-Seob Han, 한재흥

    ISSN: 2093-274X, 2093-2480
    Published: 한국항공우주학회 01.12.2018
    “…The aerodynamic benefit for conventional vortex generator (VG) is often counterbalanced by the appearance of parasite drag. An immovable installation similar…”
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    Journal Article
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    Artificial Neural Networks-Based Mission Planning Mechanism for Spacecraft by Zhaoyu Li, Rui Xu, Pingyuan Cui, Shengying Zhu

    ISSN: 2093-274X, 2093-2480
    Published: 한국항공우주학회 01.03.2018
    “…The ability to plan and react fast in dynamic space environments is central to intelligent behavior of spacecraft. For space and robotic applications, many…”
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    Genetic Algorithm Based Decentralized Task Assignment for Multiple Unmanned Aerial Vehicles in Dynamic Environments by Choi, Hyun-Jin, Kim, You-Dan, Kim, Hyoun-Jin

    ISSN: 2093-274X, 2093-2480
    Published: 한국항공우주학회 2011
    “…Task assignments of multiple unmanned aerial vehicles (UAVs) are examined. The phrase “task assignment” comprises the decision making procedures of a UAV…”
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    Journal Article
  7. 7

    Multi-Point Aerodynamic Design Optimization of DLR F-6 Wing-BodyNacelle-Pylon Configuration by Takashi Saitoh, 김형진, Keizo Takenaka, Kazuhiro Nakahashi

    ISSN: 2093-274X, 2093-2480
    Published: 한국항공우주학회 01.09.2017
    “…Dual-point aerodynamic design optimization is conducted for DLR-F6 wing-body-nacelle-pylon configuration adopting an efficient surface mesh movement method for…”
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  8. 8

    Modeling and Parameter Identification of the Slung Load System of an Unmanned Rotorcraft using a Flexible Cable by Lee, Byung-Yoon, Moon, Gun-Hee, Lee, Dong-Yeon, Tahk, Min-Jea, Oh, Hyun-Shik

    ISSN: 2093-274X, 2093-2480
    Published: 한국항공우주학회 01.06.2017
    “…In this paper, we propose a method to identify the parameters of a rotorcraft slung load system using the modal characteristics of a flexible cable. The…”
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  9. 9

    Coupled Analysis of Thermo-Fluid-Flexible Multi-body Dynamics of a Two-Dimensional Engine Nozzle by Eun, WonJong, Kim, JaeWon, Kwon, Oh-Joon, Chung, Chanhoon, Shin, Sang-Joon, Bauchau, Olivier A.

    ISSN: 2093-274X, 2093-2480
    Published: 한국항공우주학회 01.03.2017
    “…Various components of an engine nozzle are modeled as flexible multi-body components that are operated under high temperature and pressure. In this paper, in…”
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    Journal Article
  10. 10

    Unsteady Aerodynamic Characteristics depending on Reduced Frequency for a Pitching NACA0012 Airfoil at Re_c=2.3X10^4 by 김동하, 장조원, 손명환

    ISSN: 2093-274X, 2093-2480
    Published: 한국항공우주학회 01.03.2017
    “…Most of small air vehicles with moving wing fly at low Reynolds number condition and the reduced frequency of the moving wing ranges from 0.0 to 1.0. The…”
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    Journal Article
  11. 11

    Development of a new free wake model using finite vortex element for a horizontal axis wind turbin by 신형기, 박지웅, 이수갑

    ISSN: 2093-274X, 2093-2480
    Published: 한국항공우주학회 01.03.2017
    “…The treatment of rotor wake has been a critical issue in the field of the rotor aerodynamics. This paper presents a new free wake model for the unsteady…”
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  12. 12
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    Application of the Laplace transformation for the analysis of viscoelastic composite laminates based on equivalent single-layer theories by Sy, Ngoc Nguyen, Lee, Jaehun, Cho, Maenghyo

    ISSN: 2093-274X, 2093-2480
    Published: 한국항공우주학회 2012
    “…In this study, the linear viscoelastic response of a rectangular laminated plate is investigated. The viscoelastic properties,expressed by two basic…”
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    Improvement of a Low Cost MEMS Inertial-GPS Integrated System Using Wavelet Denoising Techniques by Kang, Chang-Ho, Kim, Sun-Young, Park, Chan-Gook

    ISSN: 2093-274X, 2093-2480
    Published: 한국항공우주학회 01.12.2011
    “…In this paper, the wavelet denoising techniques using thresholding method are applied to the low cost micro electromechanical system (MEMS)-global positioning…”
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  17. 17

    Active and Morphing Aerospace Structures–A Synthesis between Advanced Materials, Structures and Mechanisms by Baier, Horst, Datashvili, Leri

    ISSN: 2093-274X, 2093-2480
    Published: 한국항공우주학회 2011
    “…Active and shape morphing aerospace structures are discussed with a focus on activities aimed at practical implementation. In active structures applications…”
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  18. 18

    Structural Performance Tests of Down Scaled Composite Wind Turbine Blade using Embedded Fiber Bragg Grating Sensors by Kim, Sang-Woo, Kim, Eun-Ho, Rim, Mi-Sun, Shrestha, Pratik, Lee, In, Kwon, Il-Bum

    ISSN: 2093-274X, 2093-2480
    Published: 한국항공우주학회 01.12.2011
    “…In this study, the structural performance tests, i.e., static tests and dynamic tests of the composite wind turbine blade, were carried out by using the…”
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  19. 19

    Flutter Control of a Lifting Surface via Visco-Hysteretic Vibration Absorbers by Lacarbonara, Walter, Cetraro, Marek

    ISSN: 2093-274X, 2093-2480
    Published: 한국항공우주학회 01.12.2011
    “…In this paper, a visco-hysteretic vibration absorber (VA) is proposed to increase the flutter speed of an airfoil and enhance damping in the pre- and…”
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  20. 20

    Time-Delay Control for Integrated Missile Guidance and Control by Park, Bong-Gyun, Kim, Tae-Hun, Tahk, Min-Jea

    ISSN: 2093-274X, 2093-2480
    Published: 한국항공우주학회 2011
    “…In this paper, integrated missile guidance and control systems using time-delay control (TDC) are developed. The next generation missile requires that an…”
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    Journal Article