Computational simulation of gas turbines: Part I - Foundations of component-based models

Proceedings of the ASME Turbo Expo

Volumn 1, Issue , 1999, Pages

  Reed, John A ^a   Afieh, Abdollah A ^a  

^a Toledo   (United States)

Author keywords

Computational simulation; Gas turbines; Object oriented modeling

Indexed keywords

AIRCRAFT ENGINES; AIRCRAFT PROPULSION; COMPUTER SOFTWARE; ENGINES; GASES; HIERARCHICAL SYSTEMS; MACHINE DESIGN; MARINE ENGINES; OBJECT ORIENTED PROGRAMMING; PHASE INTERFACES; PROPULSION; TURBINE COMPONENTS;

AEROSPACE PROPULSION SYSTEM; COMPONENT-BASED MODELS; COMPUTATIONAL SIMULATION; HIERARCHICAL DECOMPOSITIONS; MULTI-FIDELITY ANALYSIS; OBJECT ORIENTED DOMAINS; OBJECT ORIENTED MODEL; STANDARDIZED INTERFACES;

GAS TURBINES;

EID: 84928560943     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/99-GT-346     Document Type: Conference Paper

References (24)

1. Arnold, K. and Gosling, 1, 1996, -The Java Programming Language" Addison Wesley Publishing Company, Inc.. Reading, MA.
2. Booth, G. 1991, "Object Oriented Design with Applications," The Benjamin/ Cummings Publishing Company, Inc., New York, NY.
3. Claus, R. W., Evans, A. L., Lytle, J. K., and Nichols. L. D. 1991, "Nuntical Propulsion System Simulation?' Computing Systems in Engineering. Vol. 2, pp. 357-364
4. Claus, R. W., Eats, A. L., and Fallen, G.J.. 1992, "Multidisciplinary Propulsion Simulation using NPSS," AIAA Papa No. 92-4709,
5. Daniele, C. J., Krosel, S. M.. Szuch, J. R. and Westakamp. Li.. 1983, "Digital Computer Program for Generating Dynamic Engine Models (DIGTEM)," NASA TM-83446.
6. Davis, D. Y., and Stearns. EM., 1985, "Energy Efficient Engine-Flight Propulsion System Final Design and Analysis?' NASA CR-I68219.
7. Drummond, C., Pollen, G., and Cannon, M., 1994, "Object-Oriented Technology for Compressor SimuLation:' AIAA Paper No. 94-3095.
8. Evans, A., Lytle, J., Fallen, G., Lopez, I., 1997, "An Integrated Computing and Interdisciplinary Systems Approach to Acropropulsion Simulation," ASME Paper No. 97-GT-303.
9. Fawke, A. J., Saravanamuttoo, H. I. H.. and Holmes, M., 1972, "Experimental Verification of a Digital Computer Simulation Method for Predicting Gas turbine Dynamic Behavior?' The Institution of Mechanical Engineers Cornhistion Engines Group, Vol. 186. pp. 32.
10. Fishwick P. A. and Zeigler, B. P. 1992. "A Muliimodel Methodology for Qualitative Model Engineering," ACM Transactions on Modeling and Computer Simulation, Vol. 12, pp. 52-81.
11. Fishwicle P. A.. 1997. "Computer Simulation: Growth through Extension?' TRANSACTIONS or The SCS, Vol 14, pp. 13-23.
12. Gamma. E., Helm. R. Johnson, R., and Vlissides..J., 1995. "Design Patterns: ektants of reusable object-oriented software." Addison Wesley Publishing Company, Inc.. Reading, MA.
13. Hall, E. J. and Delaney, R. A.. 1995. "Investigation of Advanced Counterrotation Blade Configuration Concepts for High Speed Turboprop Systems: Task VII-ADPAC Users Manual?' NASA CR 195472.
14. Holt. G., and Phillips, R., 1991, "Object-Oriented Programming in NPSS Phase 11 Report." NASA CR-NAS3-2595 I.
15. Jonsson, A., 1997, "Re-Engineering the Design Process through Computation?' ARA Paper No. 97-0641.
16. Koenig, R. W. and Fishbach. L. H., 1972, GENENG A Program for Calculating Design and Off-Design Performance of Turbojet and Turbofan Engines," NASA TN D-6552.
17. Reed. J. A.. 1998. "Onyx: An Object-Oriented Framework for Computational Simulation of Gas Turbine Systems?' Ph.D. dissertation, The University of Toledo. Toledn, Ohio.
18. Schlichting, H., 1979, "Boundary-layer theory: 7th ed," McGraw-Hill, New York.
19. Sthobeiri, T., 1986, "A General Computational Method for Simulation and Radiation of Transient Behavior of Gas Turbines?' ASME Paper No. 86-UT- ISO.
20. Snyder, A., 1986, "Encapsulation and inheritance in object-oriented languages?' In Object-Oriented Programming, Systems, Languages, and Applications Conference Proceedings, pp. 38-45, Portland, OR.
21. Seidner, K., Mihailowe, J. R.. and Blaha. R. J., 1972, "Generalized Simulation Technique for Turbojet Engine System Analysis?' NASA TN D-6610.
22. Seller,D, and Daniele, C. J., 1975, "DYGEN A Program for Calculating Steady- State and Transient Performance of Turbojet and Turbofan Engines?' NASA TND- 7901.
23. Stewart, M., 1995, "Axisyrrunetric Aerodynamic Numerical Analysis of a Turbofan Engine", ASME Pager No. 95-GT-338.
24. Szuch, J. R., 1974. "HYDES - A Generalized Hybrid Computer Program for Studying Turbojet or Turbofan Engine Dynamics." NASA TM X-3014.