Rolls-Royce, The jet engine, 5th ed., Rolls-Royce plc, London, England, 2005.
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.
Plencner, R.M., "Plotting Component Maps in the Navy/NASA Engine Program (NNEP) - A Method and its Usage," NASA TM 101433, 1989.
Mallett, W.E. and Groesbeck, D.E., "Effects of Compressor Interstage Bleed and Adjustable Inlet Guide Vanes on Compressor Stall Characteristics of a High-pressure-ratio Turbojet Engine at Altitude," NASA RM E55G27, 1956.
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.
Gallar, L., Arias, M., Pachidis, V. and Pilidis, P., "Compressor Variable Geometry Schedule Optimisation Using Genetic Algorithms," ASME Turbo Expo 2009, Orlando, F.L., USA, GT2009-60049, June 2009.
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.
Kim, S.J., Kim, D.H., Kim, K., Son, C.M., Kim, Y.I. and Min, S.K., "An Approach for the Integrated Performance Analysis of a Small Turbofan Engine with Variable Inlet Guide and Variable Stator Vane," Journal of the Korean Society of Propulsion Engineers, Vol. 16, No. 4, pp. 23-32, 2012.
Kim, D., Kim, S., Kim, K., Son, C., Kim, Y.I. and Min, S., "A Study on the Performance Prediction Method for an Axial Compressor with Variable Inlet Guide Vane," Journal of the Korean Society of Propulsion Engineers, Vol. 16, No. 4, pp. 1-8, 2012.
Kim, D., Kim, S., Son, C., Kim, K., Kim, M. and Min, S., "Transient Performance Prediction of an Axial Compressor Considering VIGV Operation Speeds," Journal of Mechanical Science and Technology, Vol. 28, No. 10, pp. 4099-4107, 2014.
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.
Kang, Y.S., Park, T.C., Hwang, O.S. and Yang, S.S., "Experimental Research on Multi Stage Transonic Axial Compressor Performance Evaluation," Journal of Fluid Machinery, Vol. 14, No. 6, pp. 96-101, 2011.
Steinke, R.J., "A Computer Code for Predicting Multistage Axial-Flow Compressor Performance by a Meanline Stage-Stacking Method," NASA TP 2020, 1982.
Park, T.J., Yoon, S. and Baek J.H., "Performance Prediction Comparison of Multi-Stage Axial-Compressor by Stage-Stacking Method," 2001 Korea Society for Fluid Machinery Conference, Daejeon, Republic of Korea, pp. 143-148, Nov. 2001.
Kim, J., Min, J., Cho, L., Gang, Y.S. and Cho, J., "Numerical Simulation of Steady and Unsteady High-Pressure Turbine Performance," 2013 KSAS conference, Jeongseon, Republic of Korea, pp.273-276, April 2013.
Honeywell F124 Turbofan Engine Brochure, http://www51.honeywell.com/aero/portal/Common/Documents/myaerospacecatalog-d ocuments/Defense_Brochures-documents/F124_Engine.pdf, June 2015.
NPSS Team, "NPSS User Guide Software Release: NPSS 2.4.1," Ohio Aerospace Institute, Cleveland, O.H., USA, 2012.
Bae, K., Min, C., Cheon, B., Lee, C. and Lee, D., "Control System of Turbofan Engine with Variable Inlet Guide Vane," Journal of The Korean Society for Aeronautical and Space Sciences, Vol. 42, No. 3, pp. 237-242, 2014.
Kim, M., Kim, H.H., Park, H.W., Go, J., Son, C., Kim, K. and Lee, D., "Displacement Amplification Output Device using Flexible Link," KR-A-10-2013-0093994, 2013.