1 |
Corbett, A.G., and Elder, R.L., 1976, "Mathematical Modeling of Compressor Stability in Steady and Unsteady Flow Conditions," Paper 12, AGARD-CP-177.
|
2 |
Chamblebee, C.E., Davies, Jr., M.W., and Kimzey, W.F., 1980, "A Multi-Stage Axial Flow Compressor Mathematical Modeling Technique with Application to Two Current Turbofan Compression Systems," AIAAPaper, AIAA-80-0054.
|
3 |
Gamache, R.N. and Greitzer, E.M., 1986, "Reverse Flow in Multistage Axial Compressors," AIAA-86-1747, 1986-6.
|
4 |
Day, I.J., Greitzer, E.M., and Cumpsty, N.A., 1978, "Prediction of Compressor Performance in Rotating Stall, Journal of Engineering for Power," ASME, Vol. 100, No.1, 1978-1, pp. 1-14.
DOI
|
5 |
Hosny, W.M. and Steenken, W.G., 1986, "Aerodynamic Instability of an Advanced High-Pressure-Ratio Compression Component," AIAA-86-1619.
|
6 |
Boyer, K.M. and O'Brien, W.F., 1989, "Model Prediction for Improved Recoverability of a Multistage Axial-Flow Compressors," AIAA-89-2687.
|
7 |
Copenhaver, W.W. and Okiishi, T.H., 1989, "Rotating Stall Performance and Recoverability of a High-Speed 10-Stage Axial-Flow Compressors," AIAA-89-2684.
|
8 |
Bloch, G.S., and O'Brien, W.F., 1992, "A Wide-Range Axial-Flow Compressor Stage Performance Model," ASME 92-GT-58.
|
9 |
In-house data of Mitsubishi Heavy Industries, Limited
|
10 |
Yamaguchi, N., 2103, "Analytical Study on Effects of Flow Path Layouts on the Compressor Surge Phenomena (in Japanese)," Turbomachinery, Turbomachinery Society of Japan, Vol. 41, No. 2 (2013-2), pp. 89-97.
|
11 |
Davies, Jr., M.W., and O'Brien, W.F., 1987, "A Stage-by-Stage Post-Stall Compression System Modeling Technique," AIAA- 87-2088.
|
12 |
Schobeiri, M.T., Attia, M., and Lippke, C., 1994, "GETRAN: A Generic Modularly Structured Computer Code for Simulation of Dynamic Behavior of Aero- and Power Generation Gas Turbine System," Journal of Engineering for Gas Turbine and Power, Transaction of the ASME, Vol. 116, 1994-7, pp. 483-494.
DOI
ScienceOn
|
13 |
Badmus, O.O, Chowdhury, S., Eveker, K.M., and Nett,C.N., 1995, "Control-Oriented High-Frequency Turbomachinery Modeling: Single-Stage Compressor System One-Dimensional Model," Journal of Turbomachinery, Transaction of the ASME, Vol. 117, 1995-1, pp. 47-61.
DOI
|
14 |
Schobeiri, M., 2004, "Turbomachinery Flow Physics and Dynamic Performance," Springer.
|
15 |
Yamaguchi, N., 2012, "A Study on the Stagnation-Stall Boundaries Based on Analytically-Evaluated Surge Conditions in Axial Flow Compressors," No. ISUAAAT13-S5-1, The 13th International Symposium on Unsteady Aerodynamics, Aeroacoustics and Aeroelasticity of Turbomachinery, 2012-9.
|
16 |
Yamaguchi, N., 2013, "Analytical Study on Stall Stagnation Boundaries in Axial Compressor and Duct System," International Journal of Fluid Machinery and Systems, Vol. 6, No. 2, April-June 2013, pp.56-74.
DOI
ScienceOn
|
17 |
Editing Committee of CFD, 1995, "Analysis of Compressible Flows (in Japanese)," Computational Fluid Dynamics Series, Vol.2, Tokyo University Press, pp. 40, and 54-55.
|
18 |
Tanahashi, T., 1993, "Dynamic Features in Flow-paths (3) (in Japanese)," Sciences of Machines, Vol. 45, No. 10, pp.1059-1060.
|
19 |
Yamaguchi, N., 2011, "Surge Transient Flow Phenomena in a Multistage Axial Flow Compressor-Duct System Predicted by a Stage-by-Stage Simulation Method, Part I Development of Simulation Code "SRGTRAN" (in Japanese)," Research Bulletin of Faculty of Sciences and Engineering, Meisei University, No. 47, 2011-3, pp. 73-85.
|
20 |
Fujii, S., 1947, "Stability and Surging in Centrifugal Pumps, Part 1 and Part 2 (in Japanese)," Transaction, Japan Society of Mechanical Engineering, Vol. 13, No. 44, 1947-5, pp. 184-191and 192-201.
DOI
|
21 |
Katto, Y., 1960, "Some Fundamental Natures of Resonant Surge, 1st Report and 2nd Report (in Japanese)," Vol. 26, No. 162, 1960-2, pp. 256-264 and pp. 265-273.
|
22 |
Greitzer, E. M., 1976, "Surge and Rotating Stall in Axial Flow Compressors, Part I and II," ASME, Journal of Engineering for Power, Vol. 98, 1976-4, pp. 190-198 and 199-217.
DOI
|