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Showing results 1 to 43 of 43

Issue Date	Title / Author(s) / Citation	File
2001	개의 하대정맥과 대동맥에서 나이티놀 스텐트의 조직 반응에 대한 비교연구 신상준	link
2007	(The)Effect of the blade nonlinear deflection upon fluid-structure interaction analysis in helicopters 김경환	link
2008-09	Coupled CFD/CSD Analysis of a Hovering Rotor Using High Fidelity Unsteady Aerodynamics and a Geometrically Exact Rotor Blade Analysis Lee, Hyun-ku; Yoon, Sung-Hwan; Shin, SangJoon; Kim, Chongam 34th European Rotorcraft Forum, Liverpool, UK, Sep. 16-19, 2008	view file
2009	Aeroelastic stability analysis of tiltrotor aircrafts with unsteady aerodynamic effect 김태성	link
2009-01	Simvastatin plus irinotecan, 5-fluorouracil, and leucovorin (FOLFIRI) as first-line chemotherapy in metastatic colorectal patients: a multicenter phase II study Lee, Jeeyun; Jung, Kyung Hae; Park, Young Suk; Ahn, Joong Bae; Shin, Sang Jun; Im, Seock-Ah; Oh, Do Youn; Shin, Dong Bok; Kim, Tae Won; Lee, Namsu; Byun, Jae Ho; Hong, Yong Sang; Park, Joon Oh; Park, Se Hoon; Lim, Ho Yeong; Kang, Won Ki Cancer Chemother Pharmacol. 2009 Sep;64(4):657-63. Epub 2009 Jan 24.	link
2010	회전익 항공기 최신 개념설계 프로그램 개발 임재훈	link
2011-02	저진동 헬리콥터 실현을 위한 지능형 능동 뒷전 플랩 로터 블레이드의 설계 이재환	link
2011-02	동체의 유연성을 고려한 회전익 항공기 하중해석 프로그램 개발 곽진성	link
2012-02	고세장비 날개의 조종면 역전 및 발산 해석 윤남경	link
2012-02	다물체 동역학을 고려한 무베어링 로터 시스템의 하중해석 전태영	link
2012-02	Aeroelastic Analysis for Turbine Blades based on the Transformation Techniques 이일	link
2013-02	헬리콥터 동적 구성품을 고려한 로터 시스템의 하중 해석 조해성	view file
2014-02	Development of an Improved Domain Decomposition Approach using Lagrange Multipliers for Large-scale Structural Analysis 곽준영	view file
2014-08	Development of Rotor Structural Design Optimization Framework for Compound Rotorcrafts with a Lift Offset 임재훈	view file
2014-11	S-1 plus oxaliplatin versus capecitabine plus oxaliplatin for the first-line treatment of patients with metastatic colorectal cancer: updated results from a phase 3 trial Kim, Seung Tae; Hong, Yong Sang; Lim, Ho Yeong; Lee, Jeeyun; Kim, Tae Won; Kim, Kyu-Pyo; Kim, Sun Young; Baek, Ji Yeon; Kim, Jee Hyun; Lee, Keun-Wook; Chung, Ik-Joo; Cho, Sang-Hee; Lee, Kyung Hee; Shin, Sang Joon; Kang, Hye Jin; Shin, Dong Bok; Lee, Jae Won; Jo, Sook Jung; Park, Young Suk BMC Cancer, 14(1):883	view file DOI
2015-02	Study on structural dynamic characteristics of rotating composite blades using three dimensional finite elements 기영중	view file
2015-02	고속 비행 환경에서의 압전 지능형 조종익 성능 개선 노인선	view file
2015-02	Design improvements of the smart active trailing-edge flap (ATF) for rotating test 강정표	view file
2016-02	Design for Flapping Wing Micro Vehicle Using 6-Bar Linkage Mechanism 전재혁	view file
2016-02	Structural Modeling and Dynamic Analysis Reflecting Liquid Propellant for Longitudinal Dynamic Instability (POGO) of Aerospace Vehicles 김준범	view file
2016-02	Transient Flow Analysis and Static Bench Measurements for an Active Trailing-Edge Flap 움베르토	view file
2016-03	6절 링크 방식의 날갯짓 초소형 비행체 설계 및 실험 이준희; 김영환; 전재혁; 신상준; 김종암 2016 제31회 제어로봇시스템학회 학술대회, pp. 15-16	view file
2016-08	PI Controller Design and Aeroservoelastic Analysis of a Smart Fin Including Piezoelectric Actuator for Performance Improvement 강유진	view file
2017-02	Prediction on the Excitation Loads and Vibratory Response of the Supersonic Flight Vehicle with Air Breathing Inlet 김진형	view file
2017-02	Development of Co-rotational Finite Elements and Application for Fluid-Structure Interaction in Biomimetic Flexible Wing Haeseong Cho	view file
2017-02	Structural Design and Analysis of All-moving Type Smart Fin using Single-crystal Piezoelectric Actuator 박철우	view file
2017-02	Development of the snapshot method for six degree-of-freedom flight dynamics simulation for a high aspect ratio wing aerial vehicle 빈영빈	view file
2017-02	Structural Dynamic Analysis of Space Launch Vehicle using Axisymmetric Shell Element including Hydroelastic Effect for Pogo Stability Analysis JiSoo Sim	view file
2017-08	측면하중 예측을 위한 발사체 엔진 노즐 3차원 고정밀 구조해석 개발 김세일	view file
2018-02	Development of a Precision Vibration Analysis Framework for Structural Safety Prediction of Gas Turbine Blades 김용세	view file
2018-02	Prediction on Pogo Phenomenon of a Space Launch Vehicle using the Virtual Mass and Modified Finite Element Method 이상구	view file
2018-02	Analytical and Experimental Evaluation of an Active Trailing-edge Flap (ATF) for Vibratory Loads Reduction in Rotorcraft 은원종	view file
2019-02	Coupled Analysis for 6-DOF Dynamics of UAV and Modified Blade Element Momentum Theory considering Gust and Flight Conditions 박선후	view file
2019-02	Experimental Evaluation and On-Blade Trailing-Edge Flap Control Algorithm for Helicopter Vibration Reduction 임병욱	view file
2019-02	Development of Computationally Affordable Flutter and Limit Cycle Oscillation Analysis using Potential-based Equations 이시훈	view file
2020	Acoustic Prediction and Measurement on Unheated Supersonic Jet Flow : Application for Small Scale Nozzle and Launch System 강승훈	view file link
2020	Research on Establishing Fatigue Evaluation Procedures of Composite Structures Using Load Enhancement Factor Approach 이창배	view file link
2021	Design of the Main Wing in Co-axial Compound Rotorcraft Considering Whirl Flutter Stability 염제완	view file link
2021-02	Pogo Instability Analysis of a Clustered Liquid Rocket with Sophisticated Branch Feedline 유정욱	view file link
2021-02	Integrated Design of Tailless FWMAV with free play: Approach via Geometry and Numerical Analysis 최재원	view file link
2021-02	Optimal Design of Wind Turbine Blade considering Multiple Variables using the Response Surface Method 이상래	view file link
2021-02	Structural responses due to the aero-acoustic pressure generated from a small-scale supersonic jet 주현식	view file link
2021-03	날갯짓 초소형 비행체의 앞전 및 시맥 탄성이 공력 성능에 미치는 영향 윤상훈; 조해성; 신상준; 허석행; 구지훈; 유재관; 김종암 한국항공우주학회지, Vol.49 No.3, pp.185-195	DOI

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