Recent advances in the development of combustor design tools

39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Volumn , Issue , 2003, Pages

  Mongia, Hukam C ^a  

^a GE AVIATION   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ANNULAR COMBUSTOR; CALCULATION APPROACHES; COMBUSTION RESEARCH; COMBUSTION SYSTEMS; COMBUSTOR DESIGNS; DIFFUSION SYSTEMS; DRY LOW EMISSIONS; PREDICTION CAPABILITY;

COMBUSTION; DOMES; MIXERS (MACHINERY); PROPULSION; TOOLS; TUBES (COMPONENTS);

COMBUSTORS;

EID: 84897585752     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (33)

1. Mongia, H. C., and Smith, K. F., 1978, "An empirical/analytical design methodology for gas turbine combustor", AIAA Paper 78-998.
2. Mongia, H. C., Reynolds, R. S., Coleman, E., and Bruce, T. W., 1979, "Combustor Design Criteria Validation Volume I-Element tests and model validation", USARTL-TR-78-55A (AD-AO-67657).
3. Mongia, H. C., Reynolds, R. S., Coleman, E., and Bruce, T. W., 1979, "Combustor Design Criteria Validation Volume II-Development testing of two full-scale annular gas turbine combustors", USARTLTR-78-55B (AD-AO-67689).
4. Mongia, H. C., and Reynolds, R. S., 1979, "Combustor Design Criteria Validation Volume III-User's Manual", USARTL-TR-78-55C (AD-AO-66793).
5. Mongia, H. C., 2001, "A Synopsis of Gas Turbine Combustor Design Methodology Evolution of Last 25 Years", ISABE 2001 Conference.
6. Mongia, Hukam C., 2001, "Gas turbine combustor liner wall temperature calculation methodology, " AIAA 2001-3267.
7. Danis, A. M., Burrus, D. L., and Mongia, H. C., 1996, "Anchored CCD for gas turbine combustor design and data correlation", J. Eng. Gas Turbines and Power, 1997, Vol. 119, pp. 535-545.
8. Mongia, Hukam C., 2003, "TAPS-A 4th Generation Propulsion Combustor Technology for Low Emissions, " International Air & Space Symposium and Exposition, The Next 100 Years, Dayton, 14-17 July, 2003, AIAA Paper 2003-2657.
9. Barlow, R. S., et al., 2002, Sixth Int. Workshop on Measurement and Computation of Turbulent Nonpremixed Flames, TNF6 18-20 July, 2002, Sapporo, Japan.
10. Keck, O., Meier, W., Stricker, W., and Aigner, M., 2002, Establishment of a confined swirling natural gas/air flame as a standard flame: Temperature and species distributions from laser Raman measurements, CST, v174(8), pp. 117-152.
11. Held, T. J, Mueller, M. A., S.-C. Li, S.-C., and Mongia, H. C., 2001, " A Data-Driven Model for NOX, CO and UHC emissions for a Dry Low Emissions Gas Turbine Combustor, " AIAA Paper 2001-3425.
12. Li, S. C., Stevens, E., and Mongia, "Application of laminar partially premixed flame model to gas turbine combustors, " ISABE 2003.
13. Li, G., Angier, S., Lambolez, O., Gutmark, E., and Drouin, B., 2002, "Experimental study of velocity flow field for a multiple swirl spray combustor, " AIAA Paper 2002-0618.
14. Grinstein, F. F. et al, 2002, " Flow dynamics in a swirling jet combustor, " Journal of Turbulence.
15. Richards, G. and Maloney, D., Private communication, November 2001.
16. Mongia, H. C., et al, 2001, "Swirl cup modeling Part 1, " AIAA Paper 2001-3576.
17. Cai, J., Fu, Y., Elkady, A., Jeng, S., and Mongia, H., 2003, "Swirl cup modeling, Part 6: Effect of confinement, " AIAA Paper 2003-0486.
18. Hsiao, G., Mongia, H., and Vij, A., 2003, "Swirl cup modeling, Part 2: Inlet conditions", AIAA Paper 2003-1350.
19. Hsiao, G., and Mongia, H., 2003, "Swirl cup modeling, Part 3: Grid independent solution with different turbulence models, " AIAA Paper 2003-1349.
20. Wang, S., and Yang, V., 2003, "Swirl cup modeling, Part 5: Large eddy simulation of cold flow, " AIAA Paper 2003-0485.
21. Kim, W-W. Menon, S., and Mongia, H.C., "Large eddy simulations of reacting flow in a dump combustor, " Combust. Sci. and Tech., 143, pp. 25-62 (1999).
22. Hura, H. S., Joshi, N. D., Mongia, H. C., and Tonouchi, J., 1998, "Dry Low Emissions Premixer CCD modeling and validation, " ASME Paper 98-GT-444.
23. Grinstein, F. F., Young, T. R., Li, G., Gutmark, E. J., Hsiao, G., and Mongia, H. C., 2001, "Flow dynamics in a swirling jet combustors, " Turbulent Shear Flow Conference.
24. Nikjoo, M., and Mongia, H., 1999, "Predictions of flows with adverse pressure gradients, " AIAA Paper 99-2817.
25. FLUENT 6.0 Training Notes, p. 6-14, January 2002.
26. Giridharan, M., Mongia, H., and Singh, G., 2003, "Scaling of dilution hole inlet conditions for gas turbine combustor CFD models, " AIAA Paper 2003-1203.
27. Hsiao, G., and Vij, A., Private communication, 2003.
28. Karki, K. C., Oechsle, V. L., and Mongia, 1992, "A computational procedure for diffuser-combustor flow interaction analysis", J. Eng. Gas Turbines and Power, January 1992, Vol. 114, pp. 1-7.
29. Mongia, H. C. et al, 2004, "On Combustor diffuser modeling to get good agreement for CP, " Future publication.
30. Giridharan, M., Private communication, 2003.
31. Rizk, N. K., and Mongia, H. C., 1992, "Semianalytical fuel injector performance correlation approach", Int. J. Turbo and Jet Engines, Vol. 9, pp. 205-213.
32. Rizk, N. K., and Mongia, H. C., 1992, "Calculation approach validation for airblast atomizers", J. Eng. Gas Turbines and Power, April 1992, Vol. 114, pp. 386-393.
33. Rizk, N. K., and Mongia, H. C., 1991, "Model for airblast atomization", J. Propulsion and Power, Vol. 7, n. 3, May-June 1991, pp. 305-311.