가변 안내익 및 정익을 가지는 소형 터보팬 엔진의 성능예측을 위한 통합 해석법 연구

목차 (Table of Contents)

• ABSTRACT
• 요약
• 1. 서론
• 2. 엔진 성능해석 모델링
• 3. 축류 압축기 탈설계 성능예측
• 4. 통합프로그램을 통한 엔진 성능 모사
• 5. 결론
• 후기
• 참고문헌

참고문헌 (Reference)

1 최원, "항공기 개념설계를 위한 가스터빈 엔진 성능 모델 연구" 2010

2 한국항공우주연구원, "차세대 소형/고부하 압축기 다분야 통합 기술 개발" KATRA 2010

3 송태원, "단축적법의 개선에 의한 축류압축기의 효과적인 성능예측" 24 (24): 1077-1084, 2000

4 박태진, "단 축적법을 이용한 다단 축류 압축기 성능예측" 789-794, 2001

5 Urasek, Donald C., "Stalled and Stall-Free Performance of Axial-Flow Compressor Stage with Three Inlet Guide-Vane and Stator-Blade Settings" NASA 1977

6 Jones, B. A., "Single stage experimental evaluation of variable geometry inlet guide vanes and stator blading, part 6 Final report" NASA 1970

7 Jones, B. A., "Single stage experimental evaluation of variable geometry guide vanes and stators. Part 3" NASA 1969

8 Jones, B. A., "Single stage experimental evaluation of variable geometry guide vanes and stators. Part 1" NASA 1968

9 Steinke, R. J., "STGSTK: A computer code for predicting multistage axial flow compressor performance by a meanline stage stacking method" NASA 1982

10 Math Works, "SIMULINK: Dynamic System Simulation for MATLAB, Ver. 2"

11 Abdollah, S., "Optimization of Variable Stator's angle for Off-design Compression system using Streamline Curvature Method" 2009

12 Follen, G., "Numerical Zooming Between a NPSS Engine System Simulation and a One-Dimensional High Compressor Analysis Code" NASA 2000

13 "NPSS training materials"

14 Edward, J. H., "NPSS Multidisciplinary Integra -tion and Analysis" NASA 2006

15 Pawl, W., "Modelling the characteristics of axial compressor of variable flow passage geometry, working in the gas turbine engine system" 14 (14): 27-32, 2007

16 "GasTurb website"

17 Cleverson, B., "Gas Turbine Performance Simulation using an Optimized Zxial Flow Compressor" 2009

18 Visser, W.P.J., "GSP, A Generic Object-Oriented Gas Turbine Simulation Environment" 2000

19 "GSP website"

20 Bilwakesh, K. R., "Evaluation of Range and Distortion Tolerence for High Mach Number Transonic Fan Stages" NASA 1971

21 John, A. R., "Development of a Prototype Simulation Executive with Zooming in the Numerical Propulsion System Simulation" NASA 1995

22 Kurzke, J., "Advanced User-friendly Gas Turbine Performance Calculations on a Personal Computer"

23 Paul, L. B., "A Method to Account for Varation of average Compressor Inlet Pressure During Instantaneous Distortion Analysis" NASA 1976