Instantaneous Flow Structures in a Reacting Gas Turbine Combustor

Instantaneous Flow Structures in a Reacting Gas Turbine Combustor

Author(s):

S. Dhanuka ( University of Michigan, Ann Arbor, MI )
J. Driscoll
H. Mongia ( General Electric Company, Cincinnati, OH )

Publication title:

AIAA meeting papers on disc

Title of ser.:

AIAA Paper : AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Ser. no.:

2008

Pub. Year:

2008

No.:

2008-4683

Paper no.:

AIAA 2008-4683

Pub. info.:

Reston, Va.: American Institute of Aeronautics and Astronautics

ISSN:

10877215

Language:

English

Call no.:

A07400/200808 [CD-ROM 2008 Disc 8]

Type:

Technical Paper

Details

TDL ID:	ZA00050885
Series ID:	PA00000151
Conf. info. (Name):	AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
Conf. info. (Number):	44th
Conf. info. (Venue):	Hartford, CT
Conf. info. (Date):	2008.07.21-2008.07.23
Note for article:	44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Hartford, CT, 21-23 July 2008

Similar Items:

1 Technical Paper The Influence of Primary Air Jets on Flow and Pollutant Emissions Characteristics within a Model Gas Turbine Combustor A. Elkady, S. Jeng, H. Mongia American Institute of Aeronautics and Astronautics	7 Technical Paper A semi-analytical finite rate two-reactor model for gas turbine combustors Tonouchi, J. H., Held, T. J., Mongia, H. C. The American Society of Mechanical Engineers
2 Technical Paper Large eddy simulations of reacting flow in a dump combustor Kim, W.-W., Menon, S., Mongia, H.C. American Institute of Aeronautics and Astronautics	8 Technical Paper AN IMPROVED METHOD FOR CORRELATION OF FILM-COOLING EFFECTIVENESS OF GAS TURBINE COMBUSTOR LINERS Li,S.C., Mongia,H.C. American Institute of Aeronautics and Astronautics
3 Technical Paper Perspective of Combustion Modeling for Gas Turbine Combustors Mongia, H. American Institute of Aeronautics and Astronautics	9 Technical Paper Application of a partially premixed laminar flamelet model to a low emissions gas turbine combustor Held, T. J., Mongia, H. C. The American Society of Mechanical Engineers
4 Technical Paper Numerical Prediction of Non-Reacting and Reacting Flow in a Model Gas Turbine Combustor. Davoudzadeh, F., Liu, N-S. American Society of Mechanical Engineers	10 Technical Paper Mixing Lengths of Reacting and Nonreacting Coaxial Injectors in a Laboratory Rocket Combustor S. Schumaker, J. Driscoll American Institute of Aeronautics and Astronautics
5 Technical Paper A Data-Driven Model for NOx, CO and UHC Emissions for a Dry Low Emissions Gas Turbine Combustor Held,T.J., Mueller,M.A., Li,S.C., Mongia,H.C. American Institute of Aeronautics and Astronautics	11 Technical Paper Emissions modeling of gas turbine combustors using a partially-premixed laminar flamelet model Held, T.J., Mongia, H.C. American Institute of Aeronautics and Astronautics
6 Technical Paper Reacting Spray Structure of a Counter-Rotating Swirl Cup. Fu, Y., Cai, J., Jeng, S.-M., Mongia, H. American Society of Mechanical Engineers	12 Technical Paper Application of RQL coal combustor technology to large utility gas turbines Wilkes, C., Wenglarz, R.A., Jart, P.J., Mongia, H.C. The American Society of Mechanical Engineers

1

2

3

4

5

6

7

8

9

10

11

12