A parametric starting study of an axial-centrifugal gas turbine engine using a one-dimensional dynamic engine model and comparisons to experimental results: Part II-simulation calibration and trade-off study

Journal of Engineering for Gas Turbines and Power

Volumn 121, Issue 3, 1999, Pages 384-393

  Owen, A K ^a   Daugherty, A ^a   Garrard, D ^b   Reynolds, H C ^c   Wright, R D ^c  

^a NASA GLENN RESEARCH CENTER   (United States)

^b JACOBS TECHNOLOGY   (United States)

^c GENERAL ELECTRIC COMPANY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; CALIBRATION; COMPUTATIONAL FLUID DYNAMICS; COMPUTER SIMULATION; GAS GENERATORS; SOCIETIES AND INSTITUTIONS; STARTING;

AERODYNAMIC TURBINE ENGINE CODE; AXIAL CENTRIFUGAL GAS TURBINE ENGINE; ONE DIMENSIONAL DYNAMIC ENGINE MODEL;

GAS TURBINES;

EID: 0032656550     PISSN: 07424795     EISSN: 15288919     Source Type: Journal    
DOI: 10.1115/1.2818485     Document Type: Article

References (4)

1. Garrard, D., Davis, M., Hale, A., Chalk, J., and Savelle, S., 1997, “Analysis of Gas Turbine Engine Operability with the Aerodynamic Turbine Engine Code,” ISABE 97-7034.
2. Garrard, G. D., Davis, M. W., Jr., and Hale, A. A., 1995, “Recent Advances in Gas Turbine Engine Dynamic Models Developed Through JDAPS,” ASME Paper 95-GT-146.
3. Fishbach, L. H., and Caddy, M. J., 1975, “NNEP: The Navy NASA Engine Program (NASA),” NASA TM-X-71857.
4. Longwell, J. P., and Weiss, M. A., 1955, “High Temperature Reaction Rates in Hydrocarbon Combustion,” Ind. Eng. Chem., Vol. 47, pp. 1634-1637