Gas turbine engine performance model applications using an object-oriented simulation tool

被引:0
作者
Alexiou, A. [1 ]
Mathioudakis, K. [1 ]
机构
[1] Natl Tech Univ Athens, Lab Thermal Turbomachines, Athens 15710, Greece
来源
Proceedings of the ASME Turbo Expo 2006, Vol 2 | 2006年
关键词
object-oriented; gas turbine; performance; simulation;
D O I
暂无
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
Engine performance models are used throughout the life cycle of an engine from conceptual design to testing, certification and maintenance. The objective of this paper is to demonstrate the use and advantages of an engine performance model, developed using an object-oriented simulation tool, for the following applications: center dot Building an engine model from existing engine components and running steady state and transient calculations center dot Development and integration of a new cooled turbine component in the existing engine model center dot Accessing the engine model from an external application center dot Using an external legacy routine in the engine model
引用
收藏
页码:109 / 116
页数:8
相关论文
共 9 条
  • [1] ALEXIOU A, 2005, GT200568678 ASME
  • [2] *EA INT, 2004, EC PRO US MAN
  • [3] Kurzke J, 2002, GT200230497
  • [4] Lakshminarayana B., 1995, Fluid Dynamics and Heat Transfer of Turbomachinery
  • [5] *RES TECHN ORG, 2002, RTOTR044
  • [6] ADAPTIVE SIMULATION OF GAS-TURBINE PERFORMANCE
    STAMATIS, A
    MATHIOUDAKIS, K
    PAPAILIOU, KD
    [J]. JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 1990, 112 (02): : 168 - 175
  • [7] STAMATIS A, 2001, 2001GT362 ASME
  • [8] TSALAVOUTAS A, 2000, 2000GT0034 ASME
  • [9] Walsh P. P., 2004, Gas Turbine Performance, V2nd ed.