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All issues Volume 20 / No 1 (2019) Mechanics & Industry, 20 1 (2019) 107 References
Open Access
Issue
Mechanics & Industry
Volume 20, Number 1, 2019
Article Number 107
Number of page(s) 18
DOI https://doi.org/10.1051/meca/2019004
Published online 04 April 2019
  1. N.A. Cumpsty, Some lessons learned, J. Turbomach. 132 (2010) 041018-1 [Google Scholar]
  2. T. Ghisu, G.T. Parks, J.P. Jarrett, P.J. Clarkson, An integrated system for the aerodynamic design of compression systems-part I: development, J. Turbomach. 133 (2011) 011011-1 [Google Scholar]
  3. T. Ghisu, G.T. Parks, J.P. Jarrett, P.J. Clarkson, An integrated system for the aerodynamic design of compression systems-Part II: application, J. Turbomach. 133 (2011) 011012-1 [Google Scholar]
  4. J.P. Jarrett, T. Ghisu, Balancing configuration and refinement in the design of two-Spool multistage compression systems, J. Turbomach. 137 (2015) 091008-1 [CrossRef] [Google Scholar]
  5. A. Sehra, J. Bettner, A. Cohn, Design of a high-performance axial compressor for utility gas turbine, J. Turbomach. 114 (1992) 277–286 [CrossRef] [Google Scholar]
  6. J.P. Smed, F.A. Pisz, J.A. Kain, N. Yamaguchi, S. Umemura, 501F compressor development program, J. Turbomach. 114 (1992) 271–276 [CrossRef] [Google Scholar]
  7. L.H. Smith, Axial compressor aerodesign evolution at general electric, J. Turbomach. 124 (2002) 321–330 [CrossRef] [Google Scholar]
  8. J.D. Mattingly, Turbomachinery, in: J.J. Corrigan, J.W. Bradley (Eds.), Elements of Gas Turbine Propulsion, International Edition, McGraw Hill Book Co., Singapore, 1996, Chap. 9, pp. 615–756 [Google Scholar]
  9. J.D. Mattingly, W.H. Heiser, D.T. Pratt, Engine component design: rotating turbomachinery, in: J.S. Przemieniecki (Ed.), Aircraft Engine Design, 2nd edn., AIAA Education Series, AIA, Reston, Virginia, USA, 2002, Chap. 8, pp. 253–324 [CrossRef] [Google Scholar]
  10. R.J. Steinke, STGSTK: A Computer Code for Predicting Multistage Axial Flow Compressor Preformance by a Meanline Stage Stacking Method, NASA Technical Paper 2020, 1982 [Google Scholar]
  11. N. Falck, Axial flow compressor mean line design, M.Sc. thesis, Department of Energy Sciences, Lund University, Lund, Sweden, 2008 [Google Scholar]
  12. D. Perrotti, Two dimensional design of axial compressor − an enhanced version of LUAX-C, M.Sc. thesis, Department of Energy Sciences, Lund University, Lund, Sweden, 2013 [Google Scholar]
  13. A. Pedersen, Ignition probability of a flammable mixture exposed to a gas turbine, Project Report for M.Sc. Programme, Department of Energy and Process Engineering, NTNU, Trondheim, Norway, 2005 [Google Scholar]
  14. GE Marine, LM2500+ marine gas turbine data sheet, GE, Cincinnati, Ohio, USA, 2006 [Google Scholar]
  15. J.F. Klapproth, M.L. Miller, D.E. Parker, Aerodynamic development and performance of the CF6-6/LM2500 compressor, in: American Institute of Aeronautics and Astronautics, 4th International Symposium on Air Breathing Engines, Orlando, FL, USA, 1979-7030 [Google Scholar]
  16. A.R. Wadia, D.P. Wolf, F.G. Haaser, Aerodynamic design and testing of an axial flow compressor with pressure ratio of 23.3:1 for the LM2500+ gas turbine, J. Turbomach. 124 (2002) 331–340 [CrossRef] [Google Scholar]
  17. R.O. Bullock, E.I. Prasse, Chapter 2 Compressor design requirements, in: I.A. Johnsen, R.O. Bullock (Eds.), Aerodynamic Design of Axial Flow Compressors, NASA SP-36, Washington D. C., USA 1965, pp. 9–51 [Google Scholar]
  18. S. Lieblein, F.C. Schwenk, R.L. Broderick, Diffusion Factor for estimating losses and limiting blade loadings in axial-flow-compressor blade elements, NACA RM E53D01, Washington D.C., 1953 [Google Scholar]
  19. J.D. Mattingly, W.H. Heiser, D.T. Pratt, Engine component design: combustion systems, in: J.S. Przemieniecki (Ed.), Aircraft Engine Design, 2nd edn., AIAA Education Series, AIAA, Reston, Virginia, USA, 2002, Chap. 9, pp. 325–418 [CrossRef] [Google Scholar]
  20. H.I.H. Saravanamuttoo, G.F.C. Rogers, H. Cohen, Axial flow compressors, in: Gas Turbine Theory, 5th edn., Dorling Kindersley (India) Pte. Ltd., Licensees of Pearson Education Ltd. in South Asia, New Delhi, India, 2001, Chap. 5, pp. 181–262 [Google Scholar]
  21. A. Pedersen, Ignition probability of a flammable mixture exposed to a gas turbine, MSc. thesis, Department of Energy and Process Engineering, NTNU, Trondheim, Norway, 2006 [Google Scholar]
  22. P.R. Holloway, G.L. Knight, C.C. Koch, S.J. Shaffer, Energy Efficient Engine High Pressure Compressor Detailed Design Report, NASA, Lewis Research Center, OH, 1982 [Google Scholar]
  23. Y.A. Cengel, Appendix 1 Property tables and charts (SI units), in: Introduction to Thermodynamics and Heat Transfer, 2nd edn., McGraw Hill, New York, USA, 2008, pp. 765–808 [Google Scholar]
  24. M.P. Boyce, Chapter 1 An overview of gas turbines, in: Gas Turbine Engineering Handbook, Butterworth-Heinemann, an imprint of Elsevier, Oxford, UK, 2012, pp. 3–87 [CrossRef] [Google Scholar]
  25. Y. Kashiwabara, Y. Matsuura, Y. Katoh, N. Hagiwara, T. Hattori, K. Tokunaga, Development of a high-pressure ratio axial flow compressor for a medium-size gas turbine, J. Turbomach. 108 (1986) 233–239 [CrossRef] [Google Scholar]
  26. I. Aartun, Using the program Allprops at the Center for Applied Thermodynamic Studies, University of Idaho, 2002. https://www.studentlitteratur.se/fileaccess/private/fid8263/ produkt/37354EnBe/torr_luft.pdf [Google Scholar]
  27. Forecast International, “www.forecastinternational.com,” November, 2010. www.forecastinternational.com/samples/F649_CompleteSample.pdf [Google Scholar]
  28. D. Bruna, C. Cravero, M.G. Turner, A. Merchant, An educational software suite for teaching design strategies for multistage axial flow compressors, J. Turbomach. 134 (2012) 051010-1 [CrossRef] [Google Scholar]
  29. S. Frei, ICAO Standard Atmosphere, Swiss Aviation Resources, 1997–2005. http://www.aviation.ch/tools-atmosphere.asp [Google Scholar]
  30. G.K. Serovy, R.P. Dring, Section 6.1 Test case E/CO-1 Single low speed compressor rotor, in: L. Fottner (Ed.), AGARD advisory report no. 275: Test cases for computation of internal flows in aero engine components, NATO AGARD Propulsion and Energetics Panel, Working Group 18, 1990, pp. 152–164 [Google Scholar]
  31. R.B. Ginder, D. Harris, Section 6.3 Test case E/CO-3 Single subsonic compressor stage, in: L. Fottner (Ed.), AGARD advisory report no. 275: Test cases for computation of internal flows in aero engine components, NATO AGARD Propulsion and Energetics Panel, Working Group 18, 1990, pp. 214–244 [Google Scholar]
  32. G.K. Serovy, R.P. Dring, Section 6.5 Test case E/CO-05 Low speed two stage compressor, in: L. Fottner (Ed.), AGARD advisory report no. 275: Test cases for computation of internal flows in aero engine components, NATO AGARD Propulsion and Energetics Panel, Working Group 18, 1990, pp. 286–298 [Google Scholar]

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