Book contents
- Reviews
- Gas Turbines for Electric Power Generation
- Gas Turbines for Electric Power Generation
- Copyright page
- Contents
- Preface
- 1 Introduction
- Part I Prerequisites
- Part II Fundamentals
- 5 Thermodynamics
- 6 Technology Factors
- 7 Heat and Mass Balance
- 8 Real Cycle Analysis
- 9 Turbine Cooling
- 10 Turbine Aero*
- 11 Compressor Aero*
- 12 Combustion
- 13 Materials
- 14 The Hardware
- Part III Extras
- Part IV Special Topics
- Book part
- Index
- References
11 - Compressor Aero*
from Part II - Fundamentals
Published online by Cambridge University Press: 15 February 2019
Book contents
- Reviews
- Gas Turbines for Electric Power Generation
- Gas Turbines for Electric Power Generation
- Copyright page
- Contents
- Preface
- 1 Introduction
- Part I Prerequisites
- Part II Fundamentals
- 5 Thermodynamics
- 6 Technology Factors
- 7 Heat and Mass Balance
- 8 Real Cycle Analysis
- 9 Turbine Cooling
- 10 Turbine Aero*
- 11 Compressor Aero*
- 12 Combustion
- 13 Materials
- 14 The Hardware
- Part III Extras
- Part IV Special Topics
- Book part
- Index
- References
- Type
- Chapter
- Information
- Gas Turbines for Electric Power Generation , pp. 265 - 307Publisher: Cambridge University PressPrint publication year: 2019
References
Smith, L. H. Jr., Axial Compressor Aerodesign Evolution at General Electric, Journal of Turbomachinery, 124 (2002), 321–330.CrossRefGoogle Scholar
Martin, R., Forry, D., Maier, S., Hansen, C., GE’s Next 7FA Gas Turbine “Test and Validation” (Schenectady, NY: GE Power & Water, 2011).Google Scholar
Benini, E., “Advances in Aerodynamic Design of Gas Turbines Compressors,” in Gas Turbines, Ed. Injeti, G. (London, UK: InTech, 2010).Google Scholar
Howell, A. R., The Present Basis of Axial Flow Compressor Design: Part 1 Cascade Theory and Performance (Richmond, UK: HM Stationery Office, 1942).Google Scholar
Denton, J. D., Loss Mechanisms in Turbomachines, Journal of Turbomachinery, 115 (1993), 621–656.Google Scholar
Hall, D. K., Greitzer, E. M., Tan, C. S., “Performance Limits of Axial Compressors,” ASME Paper GT2012-69709, ASME Turbo Expo 2012, June 11–15, 2012, Copenhagen, Denmark.Google Scholar
Becker, B., Kwasniewski, M., von Schwerdtner, O., Transonic Compressor Development for Large Industrial Gas Turbines, ASME Journal of Engineering for Power, 105 (1983), 417–421.Google Scholar
Farkas, F., “The Development of a Multi-stage Heavy-duty Transonic Compressor for Industrial Gas Turbines,” ASME Paper 86-GT-91, International Gas Turbine Conference and Exhibit, June 8–12, 1986, Düsseldorf, West Germany.CrossRefGoogle Scholar
Whitcomb, R. T., Clark, L. R., “An Airfoil Shape for Efficient Flight at Supercritical Mach Numbers,” NASA TMX-1109, May 1965.Google Scholar
Kerrebrock, J. L., Flow in Transonic Compressors, AIAA Journal, 19 (1980), 4–19.CrossRefGoogle Scholar
Hobbs, D., Weingold, H., Development of Controlled Diffusion Airfoils for Multistage Compressor Application, ASME Journal of Engineering for Gas Turbines and Power, 106 (1984), 271–278.Google Scholar
Becker, B., Schulenberg, T., Termühlen, H, “The “3A-Series” Gas Turbines With HBR® Combustors,” ASME Paper 95-GT-458, ASME 1995 International Gas Turbine and Aeroengine Congress and Exposition, June 5–8, 1995, Houston, TX.CrossRefGoogle Scholar
Köller, U., Mönig, R., Küsters, B., Schreiber, H.-A, Development of Advanced Compressor Airfoils for Heavy-Duty Gas Turbines – Part I: Design and Optimization, ASME Journal of Turbomachinery, 122 (1999), 397–405.Google Scholar
Robbins, W. H., Dugan, J. F. Jr., “Prediction of Off-Design Performance of Multistage Compressors,” in Aerodynamic Design of Axial-Flow Compressors (Washington, DC: National Aeronautics and Space Administration, 1965).Google Scholar
Nakhamkin, M., Gülen, S. C., “Transient Analysis of the Cascaded Humidified Advanced Gas Turbine (CHAT),” ASME Paper 95-CTP-28, ASME 1995 Cogen-Turbo Power Conference, August 23–25, 1995, Vienna, Austria.Google Scholar
Camp, T. R., Horlock, J. H., An Analytical Model of Axial Compressor Off-Design Performance, Journal of Turbomachinery, 116 (1994), 425–434.Google Scholar
Cumpsty, N. A., Some Lessons Learned, Journal of Turbomachinery, 132 (2010), 041018.CrossRefGoogle Scholar
Dickens, T., Day, I., The Design of Highly Loaded Compressors, Journal of Turbomachinery, 133 (2011), 031007.Google Scholar
Hall, D. K., Greitzer, E. M., Tan, C. S., “Performance Limits of Axial Compressor Stages,” ASME Paper GT2012-69709, ASME Turbo Expo 2012, June 11–15, 2012, Copenhagen, Denmark.Google Scholar
Kappis, W., “Compressors in Gas Turbine Systems,” chapter 4 in [11] in Chapter 2.Google Scholar
NASA Report SP-36, Aerodynamic Design of Axial Flow Compressors, (Washington, DC: Scientific and Technical Information Division, NASA, 1965).Google Scholar