참고문헌
- Rolls-Royce, The jet engine, 5th ed., Rolls-Royce plc, London, England, 2005.
- Peng, W.W., Fundamentals of turbomachinery, 1st ed., John Wiley & Sons, Hoboken, N.J., USA, 2008.
- Gallar, L., Arias, M., Pachidis, V. and Singh, R., "Stochastic Axial Compressor Variable Geometry Schedule Optimisation," Aerospace Science and Technology, Vol. 15, No. 5, pp. 366-374, 2011. https://doi.org/10.1016/j.ast.2010.08.010
- Evans, A.B., "The Effects of Compressor Seventh-stage Bleed Air Extraction on Performance of the F100-PW-220 Afterburning Turbofan Engine," NASA CR-179447, 1991.
- Barbosa, J.R., Silva F.J., Tomita, J.T. and Bringhenti, C., "Influence of Variable Geometry Transients on Gas Turbine Performance," ASME Turbo Expo 2011, Vancouver, Canada, GT2011-46565, June 2011.
- Bringhenti, C., Tomita, J.T., de Sousa Junior, F. and Barbosa, J.R., "Gas Turbine Performance Simulation Using an Optimized Axial Flow Compressor," ASME Turbo Expo 2006, Barcelona, Spain, GT2006-91225, May 2006.
- Shadaram, A., Fathi, A. and Azizi, R., "Optimization of Variable Stator's Angle for Off Design Compression Systems Using Streamline Curvature Method," ASME Turbo Expo 2009, Orlando, F.L., USA, GT2009-59772, June 2009.
- Curnock, B., Yin, J., Hales, R. and Pilidis, P., "High-bypass Turbofan Model using a Fan Radial-profile Performance Map," Aircraft Design, Vol. 4, No. 2, pp. 115-126, 2001. https://doi.org/10.1016/S1369-8869(01)00007-6
- Honeywell F124 Turbofan Engine Brochure, http://www51.honeywell.com/aero/portal/Common/Documents/myaerospacecatalog-documents/Defense_Brochures-documents/F124_Engine.pdf, June 2015.
- Suzuki, M. and Kuno, N., "Research and Development of Two-stage Fan Component in HYPR Project," 31st Propulsion Conference and Exhibit, San diego, C.A., USA, AIAA 95-2344, 2001.
- Garrett Turbine Engine Company, "Air Force Mixed-flow Compressor Garrett Turbine Engine Company," Report No. 21-4460-2.3, 1982.
- NPSS Team, "NPSS User Guide Software Release: NPSS 2.4.1," Ohio Aerospace Institute, Cleveland, Ohio, USA, 2012.
- Jones S.M., "An Introduction to Thermodynamic Performance Analysis of Aircraft Gas Turbine Engine Cycles Using the Numerical Propulsion System Simulation Code," NASA TM-2007-214690, 2007.
- Sellers J.F. and Daniele C.J., "DYNGEN - A Program for Calculating Steady-state and Transient Performance of Turbojet and Turbofan engines," NASA TN D-7901, 1975.
- Kim, S., Kim, D., Son, C., Kim, K., Kim, M. and Min, S., "New Profile Loss Model for Improved Prediction of Transonic Axial Flow Compressor Performance in Choking Region," ASME Turbo Expo 2015, Montreal, Canada, GT2015-42797, June 2015.
- Aungier, R.H., Axial-flow Compressors: A Strategy for Aerodynamic Design and Analysis, 1st ed., The American Society of Mechanical Engineers, New York, N.Y., USA, 2003.
- Lieblein, S., "Experimental Flow in Two-Dimensional Cascades," NASA SP-36, pp.183-226, 1965.
- Hu, J.F., Zhu, X.C., OuYang, H., Qiang, X.Q. and Du, Z.H., "Performance Prediction of Transonic Axial Compressor Based on Streamline Curvature Method," Journal of mechanical science and technology, Vol. 25, No. 12, pp. 3037-3045, 2011. https://doi.org/10.1007/s12206-011-0817-x
- Wright, P.I. and Miller, D.C., "An Improved Compressor Performance Prediction Model," RR-PNR-90873, 1991.
- Jansen, W. and Moffatt, W.C., "The Off-design Analysis of Axial-flow Compressors," Journal of Engineering for Power, Vol. 89, No. 4, pp. 453-462, 1967.
- Walsh, P.P. and Fletcher, P., Gas Turbine Performance, 2nd ed., Blackwell Science Ltd, Oxford, UK, 2005.
- Liu, Y., Dhingra, M. and Prasad, J.V.R., "Active Compressor Stability Management Via a Stall Margin Control Mode," Journal of Engineering for Power, Vol. 132, No. 5, pp. 051602-1-10, 2010.