무인비행체 블레이드 형상 변화에 따른 단일로터의 제자리 비행 추력성능 분석

논문상세정보
' 무인비행체 블레이드 형상 변화에 따른 단일로터의 제자리 비행 추력성능 분석' 의 주제별 논문영향력
논문영향력 선정 방법
논문영향력 요약
주제
  • 기계공학
  • bladeelementtheory(깃요소이론)
  • bladeparameters(블레이드설계인자)
  • computationalfluiddynamicssimulation(전산유체해석)
  • hovering(제자리비행)
  • multi-rotorunmannedaerialvehicle(멀티로터무인비행체)
  • thrust(추력)
동일주제 총논문수 논문피인용 총횟수 주제별 논문영향력의 평균
951 1

0.0%

' 무인비행체 블레이드 형상 변화에 따른 단일로터의 제자리 비행 추력성능 분석' 의 참고문헌

  • Towards Dynamically-Favourable Quad-Rotor Aerial Robots
    Pounds, P. Proceedings of the 2004 Australasian Conference on Robotics &Automation [2004]
  • Theory of wing sections-including a summary of airfoil data
    Abbott, I. H. Dover Publications [1959]
  • Survey of Micro air Vehicles in an International Even & Utilization in Thailand
    Thipuopas, C. The First TSME International Conference on Mechanical Engineering [2010]
  • Quad-Rotor Unmanned Aerial Vehicle Helicopter Modelling & Control
    Naidoo, Y International Journal of Advanced Robotic System 8 (4) : 139 ~ 149 [2011]
  • Optimization of Lift Force of Mini Quad Rotor Helicopter by Changing of Gap Size Between Rotors
    Aleksandrov, D. Solid State Phenomena 198 : 226 ~ 231 [2013]
  • Numerical Optimization of Helicopter Rotor Blade Design for Active Twist Control
    Kovalovs, A Taylor & Francis 11 (Issue. 3) : 3 ~ 9 [2007]
  • Modelling and Control of a Large Quadrotor Robot
    Punds, P. Control Engineering Practice 18 (7) : 691 ~ 699 [2010]
  • Incompressible/Compressible Flow Analysis over High-Lift Airfoils Using Two-Equation Turbulence Models
    Kim, C. S Korean Society for Computational Fluids Engineering 4 (1) : ~ [1999]
  • CFD Analysis of Rotor-Fuselage Interactional Aerodynamics
    Steijl, R 45th AIAA Aerospace Sciences Meeting and Exhibit : 1278 ~ [2007]
  • Aerodynamic Performance Analysis of Fan-Bladed Rotors in Tandem Arrangement
    Yun, J, H. The Korean Society of Mechanical Engineers Spring Annual Meeting : 331 ~ 334 [2012]
  • ADINA System 8.8 Release Notes
    ADINA R&D, Inc [2012]
  • A Study on the Composite Blade Performance Variation by Attaching Erosion Shield for Hovercraft
    김윤해 한국마린엔지니어링학회지 33 (7) : 1017 ~ 1025 [2009]