Effect of Swirl Injector Design and Other Important Parameters on Gas Turbine Combustion

Effect of Swirl Injector Design and Other Important Parameters on Gas Turbine Combustion

Author(s):

Brossard, C. ( The Pennsylvania State University )
Lee, S.-Y.
Mordaunt, C.
Broda, J.-C.
Santoro, R.J.

Publication title:

AIAA paper

Title of ser.:

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

Ser. no.:

2000

Pub. Year:

2000

No.:

2000-3122

Paper no.:

00-3122

Page(from):

1

Page(to):

7

Pub. info.:

American Institute of Aeronautics and Astronautics

ISSN:

01463705

Language:

English

Call no.:

A07400

Type:

Technical Paper

Details

TDL ID:	ZA00050879
Series ID:	PA00000151
Conf. info. (Name):	AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Conf. info. (Number):	36th
Conf. info. (Venue):	Huntsville, AL
Conf. info. (Date):	2000.07.16-2000.07.19
Note for article:	36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference 17-19 July 2000 Huntsville, Alabama

Similar Items:

1 Technical Paper Raman Spectroscopy Based Study of RBCC Ejector Mode Performance Lehman, M., Pal, S., Broda, J.C., Santoro, R.J. American Institute of Aeronautics and Astronautics	7 Technical Paper Predectonator to Thrust Tube Detonation Transition Studies for Multi-Cycle PDE Applications Saretto, S.R., Lee, S.-Y., Conrad, C., Brumberg, J., Pal, S., Santoro, R.J. American Institute of Aeronautics and Astronautics
2 Technical Paper Raman spectroscopy based study of RBCC ejector mode performance Lehman, M., Pal, S., Broda, J.C., Santoro, R.J. American Institute of Aeronautics and Astronautics	8 Technical Paper Deflagration to Detonation Transition Study Using Simultaneous Schlieren And OH PLIF Images Lee, S.-Y., Conrad, C., Watts, J., Woodward, R., Pal, S., Santoro, R.J. American Institute of Aeronautics and Astronautics
3 Technical Paper Applications of laser-based diagnostics to high pressure rocket and gas turbine combustor studies Santoro, R.J. American Institute of Aeronautics and Astronautics	9 Technical Paper Experimental Liquid Rocket Swirl Coaxial Injector Study Using Non-Intrusive Optical Techniques Kalitan, D., Salgues, D., Mouis, A., Lee, S., Pal, S., Santoro, R. American Institute of Aeronautics and Astronautics
4 Technical Paper Shear and Swirl Coaxial Injector Studies of LOX/GCH4 Rocket Combustion Using Non-Intrusive Laser Diagnostics D. Salgues, A. Mouis, S. Lee, D. Kalitan, S. Pal, R. Santoro American Institute of Aeronautics and Astronautics	10 Technical Paper Major species and temperature profiles of LOX/GH2 combustion Yeralan, S., Pal, S., Santoro, R.J. American Institute of Aeronautics and Astronautics
5 Technical Paper Design of efficient GO2/GH2 injectors: a NASA, industry and university cooperative effort Tucker, P.K., Klem, M.D., Smith, T.D., Farhangi, S., Fisher, S.C., Santoro, R.J. American Institute of Aeronautics and Astronautics	11 Technical Paper Experimental Study of a Pulse Detonation Engine Driven Ejector Shehadeh, R., Saretto, S., Lee, S.-Y., Santoro, R.J. American Institute of Aeronautics and Astronautics
6 Technical Paper Effect of Flow Parameter Variations on Full Coverage Film-Cooling Effectiveness for a Gas Turbine Blade. Mhetras, S., Han, J-C., Rudolph, R. American Society of Mechanical Engineers	12 Technical Paper Experimental investigation of oxygen rich LOX/GH2 combustion using linewise Raman imaging Yeralan, S., Pal, S., Santoro, R.J. American Institute of Aeronautics and Astronautics

1

2

3

4

5

6

7

8

9

10

11

12