Free 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]

Current usage metrics show cumulative count of Article Views (full-text article views including HTML views, PDF and ePub downloads, according to the available data) and Abstracts Views on Vision4Press platform.

Data correspond to usage on the plateform after 2015. The current usage metrics is available 48-96 hours after online publication and is updated daily on week days.

Initial download of the metrics may take a while.