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

著者名:

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

掲載資料名:

AIAA meeting papers on disc

シリーズ名:

AIAA Paper : Aerospace Sciences Meeting and Exhibit

シリーズ巻号:

2007

発行年:

2007

通号:

2007-0571

ペーパー番号:

AIAA Paper 2007-571

出版情報:

Reston, Va.: American Institute of Aeronautics and Astronautics

ISSN:

10877215

言語:

英語

請求記号:

A07400/200703 [CD-ROM 2007 Disc 3]

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00050742
シリーズID:	PA00000138
会議名:	AIAA Aerospace Sciences Meeting and Exhibit
回次:	45th
会議開催地:	Reno, Nevada
会議開催年:	2007.01.08-2007.01.11

類似資料:

1 テクニカルペーパー 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 テクニカルペーパー Major species and temperature profiles of LOX/GH2 combustion Yeralan, S., Pal, S., Santoro, R.J. American Institute of Aeronautics and Astronautics
2 テクニカルペーパー 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 テクニカルペーパー 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 テクニカルペーパー 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 テクニカルペーパー Combustion Instability Studies Using Gaseous Methane and Liquid Oxygen W. Marshall, S. Pal, R. Woodward, R. Santoro American Institute of Aeronautics and Astronautics
4 テクニカルペーパー 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 テクニカルペーパー 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 テクニカルペーパー 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 テクニカルペーパー 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 テクニカルペーパー 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 テクニカルペーパー 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

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