연구동향 분석

초음속 충동형 터빈 성능개선을 위한 동익 오버랩 최적설계

조종재(Jongjae Cho) 신봉근(Bong Gun Shin) 김귀순(Kuisoon Kim) 정은환(Eunhwan Jeong) 2014년

논문상세정보
인용/피인용
' 초음속 충동형 터빈 성능개선을 위한 동익 오버랩 최적설계' 의 주제별 논문영향력
논문영향력 선정 방법
논문영향력 요약
주제
  • 폭발물, 연료공업
  • approximate optimization(근사 최적화)
  • rotoroverlap(동익오버랩)
  • supersonic turbine(초음속 터빈)
  • turbopump(터보펌프)
동일주제 총논문수 논문피인용 총횟수 주제별 논문영향력의 평균
193 0

0.0%

' 초음속 충동형 터빈 성능개선을 위한 동익 오버랩 최적설계' 의 참고문헌

  • 속도 복합형 초음속 충동형 터빈의 동익 오버랩에 따른 성능특성
    조종재 한국추진공학회지 15 (1) : 19 ~ 28 [2011]
  • iSIGHT Designer’s Guide, Version FD 3.1
    Engineous Software, Inc. [2008]
  • Towards the Ultimate Conservative Difference Scheme, V : A Second-Order Sequel to Godunov’s Method
    Van Leer, B. Journal of Computational Physics 32 : 101 ~ 136 [1979]
  • Theory and Tunnel Tests of Rotor Blades for Supersonic Turbines
  • Theory and Calculation of Liquid Propellant Rocket Engine Pumps
    Ovsyanikov, B.V. Mashinostroyenie [1986]
  • Renormal ization Group Analysis of Turbulence. 1. Basic Theory
    Yakhot V. Journal of Science Computation 1 : 3 ~ 51 [1986]
  • Re sponse Surface Methodology - Process and Product Optimization Using Designed Ex periments
    Myers, R.H. John Wiley & Sons [1995]
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    Iman, R.L. OSTI 5571631 [1980]
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    Fluent Inc. [2004]
  • Fluent User’s Guide
    Fluent, Inc. [1998]
  • Experimental Investigation of Supersonic Turbine Performance
    Kurzrock, J.W. Gas Turbine and Aeroengine Congress and Exposition [1989]
  • Effects of Endwall Geometry and Stacking on Two-stage Supersonic Turbine Performance
    Dorney, D.J. 40th AIAA Aerospace Sciences Meeting [2002]
  • Development Status of a Turbopump for 30-ton Thrust Level of Engine
    Kim, J.H. 2005 the Korean Society of Propulsion Engineers Fall Conference : 375 ~ 383 [2005]
  • Design and Experimental Investigation of a Single-stage Turbine with a Rotor Entering Relative Mach number of 2
  • Calculation of Gas dynamic and Geometric Parameters of Turbine