LOX/GH2 Shear Coaxial Injector Atomization Studies at Large Momentum Flux Ratios

LOX/GH2 Shear Coaxial Injector Atomization Studies at Large Momentum Flux Ratios

著者名:

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

掲載資料名:

AIAA meeting papers on disc

シリーズ名:

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

シリーズ巻号:

2006

発行年:

2006

通号:

2006-5203

ペーパー番号:

AIAA Paper 2006-5203

出版情報:

Reston, Va: American Institute of Aeronautics and Astronautics

ISSN:

10877215

言語:

英語

請求記号:

A07400/200617 [CD-ROM 2006 Disc 17]

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00047243
シリーズID:	PA00000151
会議名:	AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
回次:	42nd
会議開催地:	Sacramento, California
会議開催年:	2006.07.09-2006.07.12

類似資料:

1 テクニカルペーパー LOX/GH2 Shear Coaxial Injector Atomization Studies: Effect of Recess and Non-Concentricity R. Woodward, S. Pal, S. Farhangi, G. Jensen, R. Santoro American Institute of Aeronautics and Astronautics	7 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
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 Major species and temperature profiles of LOX/GH2 combustion Yeralan, S., Pal, S., Santoro, R.J. American Institute of Aeronautics and Astronautics
3 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	9 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
4 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	10 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
5 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	11 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
6 テクニカルペーパー Chamber Wall Heat Flux Measurements for a LOX/CH4 Propellant Uni-Element Rocket J. Locke, S. Pal, R. Woodward American Institute of Aeronautics and Astronautics	12 テクニカルペーパー 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

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