LOX/GH2 Shear Coaxial Injector Atomization Studies: Effect of Recess and Non-Concentricity

LOX/GH2 Shear Coaxial Injector Atomization Studies: Effect of Recess and Non-Concentricity

Author(s):

R. Woodward ( Pennsylvania State University, University Park, PA )
S. Pal
S. Farhangi ( Pratt & Whitney Rocketdyne, Canoga Park, CA )
G. Jensen ( Pennsylvania State University, University Park, PA )
R. Santoro

Publication title:

AIAA meeting papers on disc

Title of ser.:

AIAA Paper : Aerospace Sciences Meeting and Exhibit

Ser. no.:

2007

Pub. Year:

2007

No.:

2007-0571

Paper no.:

AIAA Paper 2007-571

Pub. info.:

Reston, Va.: American Institute of Aeronautics and Astronautics

ISSN:

10877215

Language:

English

Call no.:

A07400/200703 [CD-ROM 2007 Disc 3]

Type:

Technical Paper

Details

TDL ID:	ZA00050742
Series ID:	PA00000138
Conf. info. (Name):	AIAA Aerospace Sciences Meeting and Exhibit
Conf. info. (Number):	45th
Conf. info. (Venue):	Reno, Nevada
Conf. info. (Date):	2007.01.08-2007.01.11

Similar Items:

1 Technical Paper LOX/GH2 Shear Coaxial Injector Atomization Studies at Large Momentum Flux Ratios R. Woodward, S. Pal, S. Farhangi, R. Santoro American Institute of Aeronautics and Astronautics	7 Technical Paper Major species and temperature profiles of LOX/GH2 combustion Yeralan, S., Pal, S., Santoro, R.J. American Institute of Aeronautics and Astronautics
2 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	8 Technical Paper Experimental Study of Transverse Combustion Instabilities in a Multi-Element, Rectangular Rocket Chamber W. Marshall, S. Pal, R. Woodward, R. Santoro American Institute of Aeronautics and Astronautics
3 Technical Paper Injector research for shuttle OMS upgrade using LOX/ethanol propellants Woodward, R.D., Miller, K.L., Bazarov, V.G., Guerin, G.F., Pal, S., Santoro, R.J. American Institute of Aeronautics and Astronautics	9 Technical Paper Combustion Instability Studies Using Gaseous Methane and Liquid Oxygen W. Marshall, S. Pal, R. Woodward, R. Santoro American Institute of Aeronautics and Astronautics
4 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	10 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
5 Technical Paper Experimental and analytical characterization of a shear coaxial combusting GO2/GH2 flowfield Foust, M.J., Deshpande, M., Pal, S., Ni, T., Merkle, C.L., Santoro, R.J. American Institute of Aeronautics and Astronautics	11 Technical Paper Effects of LOx Post Recess on the Combustion Characteristics for Bi-Swirl Coaxial Injector Kim, S., Han, Y., Seo, S., Moon, I., Kim, J., Seol, W. American Institute of Aeronautics and Astronautics
6 Technical Paper Benchmark Wall Heat Flux Data for a GO2/GH2 Single Element Combustor Marshall, W., Pal, S., Woodward, R., Santoro, R. American Institute of Aeronautics and Astronautics	12 Technical Paper Comparative study of recessed and non-recessed swirl coaxial injectors Sasaki, M., Sakamoto, H., Takahashi, M., Tomita, T., Tamura, H. American Institute of Aeronautics and Astronautics

1

2

3

4

5

6

7

8

9

10

11

12