Gas turbine cycle design methodology: A comparison of parameter variation with numerical optimization

Journal of Engineering for Gas Turbines and Power

Volumn 121, Issue 1, 1999, Pages 6-11

  Kurzke, J ^a  

^a AIRBUS GROUP INNOVATIONS   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

ALGORITHMS; COMPUTER SIMULATION; INTERFACES (COMPUTER); OPTIMIZATION; PERSONAL COMPUTERS; THERMAL CYCLING; TURBOFAN ENGINES;

NUMERICAL OPTIMIZATION;

GAS TURBINES;

EID: 0032625863     PISSN: 07424795     EISSN: 15288919     Source Type: Journal    
DOI: 10.1115/1.2816315     Document Type: Article

References (7)

1. Kurzke J., 1998, “Manual GasTurb 8.0 for Windows-A Program to Calculate Design and Off-Design Performance of Gas Turbines,” available from the author.
2. Jacob, H. G., 1982, “Rechnergestützte Optimierung statischer und dynamischer Systeme,” Fachberichte Messen-Steuern-Regeln, Springer-Verlag KG, Berlin.
3. Kelahan, R. C., Gaddy, J. L., 1978, “Application of the Adaptive Random Search to Discrete and Mixed Integer Optimization,” International Journal for Numerical Methods in Engineering, Vol. 12, pp. 289-298.
4. Kurzke, J., 1996, “How to Get Component Maps for Aircraft Gas Turbine Performance Calculations,” ASME Paper 96-GT-164.
5. Glassman, A. J., 1992, “Users Manual for Updated Computer Code for Axial-Flow Compressor Conceptual Design,” NASA Contractor Report 171-189.
6. Stewart, W. L., 1961, “A Study of Axial-Flow Turbine Efficiency Characteristics in Terms of Velocity Diagram Parameters,” ASME Paper 61-WA-37.
7. h ed., Addison-Wesley Longman, London, United Kingdom.