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http://dx.doi.org/10.6108/KSPE.2012.16.4.023

An Approach for the Integrated Performance Analysis of a Small Turbofan engine with Variable Inlet Guide and Variable Stator Vane  

Kim, Sang-Jo (부산대학교 대학원 항공우주공학과)
Kim, Dong-Hyun (부산대학교 대학원 항공우주공학과)
Son, Chang-Min (부산대학교 기계공학부)
Kim, Kui-Soon (부산대학교 항공우주공학과)
Kim, You-Il (국방과학연구소 1기술연구본부 5부)
Min, Seong-Ki (국방과학연구소 1기술연구본부 5부)
Publication Information
Journal of the Korean Society of Propulsion Engineers / v.16, no.4, 2012 , pp. 23-32 More about this Journal
Abstract
The present study is aimed to develop an integrated performance analysis approach for the application of a compressor with variable inlet guide vane (VIGV) and vairable stator vane (VSV) in a small turbofan engine. For the integrated analysis approach, an engine performance analysis program, NPSS and a computer program used for predicting of axial flow compressor performance based on stage stacking method, STGSTK were linked with an optimisation package, Isight. This enables off-design performance analysis for the turbofan engine with VIGV and VSV hence provides the capability to predict stable operation condition of the engine with acceptable surge margin.
Keywords
Variable Inlet Guide Vane; Variable Stator Vane; Compressor; Turbofan Engine; Engine Performance;
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  • Reference
1 Steinke, R. J., "STGSTK: A computer code for predicting multistage axial flow compressor performance by a meanline stage stacking method," NASA-TP-2020, 1982
2 Bilwakesh, K. R., "Evaluation of Range and Distortion Tolerence for High Mach Number Transonic Fan Stages," NASA CR-72787, 1971
3 Urasek, Donald C., Steinke, Ronald J. and Cunnan, Walter S., "Stalled and Stall-Free Performance of Axial-Flow Compressor Stage with Three Inlet Guide-Vane and Stator-Blade Settings," NASA TN D-8457, 1977
4 Jones, B. A., Wright, D. L., "Single stage experimental evaluation of variable geometry guide vanes and stators. Part 1," NASA CR-54556, 1968
5 박태진, 백제현, 윤성호, "단 축적법을 이용한 다단 축류 압축기 성능예측," 대한기계학회 2001년도 춘계학술대회논문집, 2001, pp.789-794
6 Paul, L. B. and Leon, M. W., "A Method to Account for Varation of average Compressor Inlet Pressure During Instantaneous Distortion Analysis," NASA TM X-73438, 1976
7 한국항공우주연구원, "차세대 소형/고부하 압축기 다분야 통합 기술 개발," KATRA08_A00133_기4, 2010
8 NPSS training materials, 2011
9 Pawl, W., "Modelling the characteristics of axial compressor of variable flow passage geometry, working in the gas turbine engine system," Marine Engineering, Vol. 14, No. 3, 2007, pp.27-32
10 Abdollah, S., Alireza, F., Ruhollah, A., "Optimization of Variable Stator's angle for Off-design Compression system using Streamline Curvature Method," ASME Turbo Expo 2009 GT2009-59772, June, 2009
11 Cleverson, B., Jesuino, T. T., Francisco de, S. J., Joao, R. B., "Gas Turbine Performance Simulation using an Optimized Zxial Flow Compressor," ASME Turbo Expo 2009 GT2009-91225, June, 2009
12 Kurzke, J., "Advanced User-friendly Gas Turbine Performance Calculations on a Personal Computer," ASME 95-GT-147
13 GasTurb website: www.gasturb.de
14 Visser, W.P.J., and Broomhead, M.J., 2002, "GSP, A Generic Object-Oriented Gas Turbine Simulation Environment," ASME 2000-GT-2
15 GSP website: www.gspteam.com
16 Math Works, 1997, "SIMULINK: Dynamic System Simulation for MATLAB, Ver. 2," The Math Works Inc., USA
17 Follen, G. and aubuchon, M., "Numerical Zooming Between a NPSS Engine System Simulation and a One-Dimensional High Compressor Analysis Code," NASA TM-2000-209913, 2000
18 John, A. R. and Abdollah, A. A., "Development of a Prototype Simulation Executive with Zooming in the Numerical Propulsion System Simulation," NASA CR-200613, 1995
19 Edward, J. H., Joseph, R., Todd, A. S., Daniel, H., "NPSS Multidisciplinary Integration and Analysis," NASA CR-2006-213890, 2006
20 최원, 유채호, 정인면, 이일우, "항공기 개념 설계를 위한 가스터빈 엔진 성능 모델 연구," 한국항공우주공학회 2010년도 춘계학술대회 논문집, 2010
21 송태원, 김재환, 김동섭, 노승탁, "단축적법의 개선에 의한 축류압축기의 효과적인 성능예측," 대한기계학회논문집 B권, Vol. 24, No. 8, 2000, pp.1077-1084
22 Jones, B. A., "Single stage experimental evaluation of variable geometry inlet guide vanes and stator blading, part 6 Final report," NASA CR-54559, 1970
23 Jones, B. A., Oscarson, R. P., "Single stage experimental evaluation of variable geometry guide vanes and stators. Part 3," NASA CR-54554, 1969