Browse > Article

The Performance Modeling of a Low Bypass Turbofan Engine for Supersonic Aircraft  

Choi, Won (한국항공우주산업(주) 고정익선행연구팀)
You, Jae-Ho (한국항공우주산업(주) 고정익선행연구팀)
Lee, Il-Woo (한국항공우주산업(주) 고정익선행연구팀)
Publication Information
Journal of the Korean Society of Propulsion Engineers / v.14, no.6, 2010 , pp. 79-88 More about this Journal
Abstract
This paper dealt with the performance modeling of a low bypass turbofan engine for supersonic aircraft. The Pratt and Whitney F100-PW-229 engine has been employed for low bypass turbofan engine performance modeling. Generally, the complete commercially-classified informations concerning the engine are unknown. The components' generic characteristics and assumptions made in order to build the F100-PW-229 engine performance model using by the published data from the open literature as basic data are described. Through the comparison of engine performance model's analysis data using Gasturb11 with engine deck data showed that the engine performance model was evaluated to be properly constructed.
Keywords
Performance Modeling; Low Bypass; Turbofan Engine; Gastur; Engine Performance;
Citations & Related Records
Times Cited By KSCI : 1  (Citation Analysis)
연도 인용수 순위
1 Applied Vehicle Technology Pane(AVT) Task Group, "Performance Prediction and Simulation of Gas Turbine Engine Operation for Aircraft, Marine, Vehicular, and Power Generation", NATO Research and Technology Organisation, 2007
2 황진석, 문희장, 구자예, "터보팬 엔진에서 터빈 냉각이 성능에 미치는 영향에 대한 수치적 해석", 한국항공운항학회지, 제14권 1호, 2006, pp.15-21   과학기술학회마을
3 David Bridges, "Thrust and Drag Models for Performance Calculations for High-Speed Aircraft", 45th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, Jan. 8-11, 2007
4 Love, C. M., "Design and Development of an Advanced F100 Compressor", AGARD CP-421, 1987
5 Joachim Kurzke, "SmoothC 8.1 user manual", 2008
6 Joachim Kurzke, "How to Create a Preformance Model of a Gas Turbine from a Limited Amount of information", Proceeding of ASME Turbo Expo 2005 Power for Land, Sea, and Air Reno-Tahoe, June 6-9, 2005
7 Aik Soon Lee, Riti Singh, S D Probert, "Modeling of the Performance of a F100-PW229 Equivalent Engine under Sea-Level Static Conditions", 45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Aug, 2-5, 2009
8 www.janes.com
9 Walsh, P. P., and Fletcher, P., "Gas-Turbine Performance", Blackwell Science, Oxford, 2004
10 Cumpsty, N. A., "Jet Propulsion: A Simple Guide to the Aerodynamic and Thermodynamic Design and Performance of Jet Engines - 2nd Edition", Cambridge University Press, UK, 2003
11 Joachim Kurzke, "Gasturb 11 user manual", 2008
12 Mattingly, J. D., "Elements of Propulsion: Gas Turbines and Rockets", American Institute of Aeronautics and Astronautics, Inc., Reston, VA, USA, 2006
13 Koff, B. L., "F100-PW-229 Higher Thrust in Same Frame Size", J. Eng. Gas Turbines Power, Volume 111 Issue 2, April, 1989