1 |
Kong, C., Ki, J. and Kang, M., "A New Scaling Method for Component Maps of Gas Turbine Using System Identification," Journal of Engineering Gas Turbines Power, Vol. 125, No. 4, pp. 979-985, 2003.
DOI
|
2 |
Petrovic, M.V., Wiedermann, A. and Banjac, M.B., "Development and Validation of a New Universal Through Flow Method for Axial Compressors.," Proceedings of ASME Turbo Expo 2009, Orlando, F.L., U.S.A., GT 2009-59938, Jun. 2009.
|
3 |
Evans, D.C. and Hill, J.M., "Experimental Investigation of a 4.5-stage Turbine with Very High Stage Loading Factor I - Turbine Design," NASA CR-2140, 1973.
|
4 |
Walket, N.D. and Tbomas, M.W., "Experimental Investigation of a 4.5-stage Turbine with Very High Stage Loading Factor II - Turbine Performance," NASA CR-2363, 1974.
|
5 |
Steinke, R.J., "A Computer Code for Predicting Multistage Axial-Flow Compressor Performance by a Meanline Stage-Stacking Method," NASA TM-2020, 1982.
|
6 |
Glassman, A.J., "Users Manual and Modeling Improvements for Axial Turbine Design and Performance Computer Code TD2-2," NASA CR-189118, 1992.
|
7 |
Flagg, E.E., "Analytical Procedure and Computer Program for Determining the Off-Design Performance of Axial Flow Turbines," NASA CR-710, 1967.
|
8 |
Glassman, A.J, "Modeling Improvements and Users Manual for Axial-Flow Turbine Off-Design Computer Code AXOD," NASA CR-195370, 1994.
|
9 |
Hendricks, E.S., "Meanline Analysis of Turbines with Choked Flow in the Object-Oriented Turbomachinery Analysis Code," 54th AIAA Aerospace Sciences Meeting, San Diego, C.A., U.S.A., AIAA 2016-0119, Jan. 2016.
|
10 |
Chen, S.S, "Capability Extension to the Turbine Off-Design Computer Program AXOD With Applications to the Highly Loaded Fan-Drive Turbines," NASA TM-2011-217129, 2011.
|
11 |
Sellers, J.F. and Daniele, C.J., "DYNGEN: A program for calculating steady-state and transient performance of turbojet and turbofan engines," NASA TN-7901, 1975.
|
12 |
Tournier, J.M. and El-Genk, M.S., "Axial Flow, Multi-Stage Turbine and Compressor Models," Energy Conversion and Management, Vol. 51, No. 1, pp. 16-29, 2010.
DOI
|
13 |
Bang, M.H., "Effect of combustor exit flow and endwall leakage flow on a multi-stage turbine system," Ms degree, School of Mechanical Engineering, Pusan National University, Pusan, Korea, 2015.
|