Diagnostic Development for Oxygen / Hydrogen Rocket Flowfield Characterization

Diagnostic Development for Oxygen / Hydrogen Rocket Flowfield Characterization

著者名:

J. Locke ( The Pennsylvania State University, University Park, PA )
S. Pal
R. Santoro

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:

2008

発行年:

2008

通号:

2008-5029

ペーパー番号:

AIAA 2008-5029

出版情報:

Reston, Va.: American Institute of Aeronautics and Astronautics

ISSN:

10877215

言語:

英語

請求記号:

A07400/200808 [CD-ROM 2008 Disc 8]

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00050885
シリーズID:	PA00000151
会議名:	AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
回次:	44th
会議開催地:	Hartford, CT
会議開催年:	2008.07.21-2008.07.23
論文注記:	44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Hartford, CT, 21-23 July 2008

類似資料:

1 テクニカルペーパー Critical issues for making droplet measurements in liquid oxygen/hydrogen combusting sprays Rahman, S., Pal, S., Santoro, R. American Institute of Aeronautics and Astronautics	7 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
2 テクニカルペーパー Experimental Investigation of the RBCC Rocket-Ejector Mode Lehman, M., Pal, S., Santoro, R. J. American Institute of Aeronautics and Astronautics	8 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
3 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	9 テクニカルペーパー Combustion Instability Studies in a Rectangular Rocket Chamber W. Marshall, S. Pal, R. Santoro American Institute of Aeronautics and Astronautics
4 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	10 テクニカルペーパー Applications of laser-based diagnostics to high pressure rocket and gas turbine combustor studies Santoro, R.J. American Institute of Aeronautics and Astronautics
5 テクニカルペーパー Gaseous propellant rocket studies using Raman spectroscopy Foust, M.J., Pal, S., Santoro, R.J. American Institute of Aeronautics and Astronautics	11 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
6 テクニカルペーパー Rocket Testing at University Facilities Santoro,R.J., Pal,S., Woodward,R.D., Schaaf,L. American Institute of Aeronautics and Astronautics	12 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

1

2

3

4

5

6

7

8

9

10

11

12