Experimental and Computational Investiagtion of Combustor Acoustics and Instabilities, Part II: Transverse Modes

Experimental and Computational Investiagtion of Combustor Acoustics and Instabilities, Part II: Transverse Modes

著者名:

R. Smith ( Purdue University, West Lafayette, IN )

W. Marshall ( Pennsylvania State University, University Park, PA )

G. Xia ( Purdue University, West Lafayette, IN )

R. Woodward ( Pennsylvania State University, University Park, PA )

S. Pal

R. Santoro

V. Sankaran ( Purdue University, West Lafayette, IN )

C. Merkle

さらに 3 件

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:

2006

発行年:

2006

通号:

2006-0538

ペーパー番号:

AIAA Paper 2006-538

出版情報:

Reston, Va.: American Institute of Aeronautics and Astronautics

ISSN:

10877215

言語:

英語

請求記号:

A07400/200602 [CD-ROM 2006 Disc 2]

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00047217
シリーズID:	PA00000138
会議名:	AIAA Aerospace Sciences Meeting and Exhibit
回次:	44th
会議開催地:	Reno, Nevada
会議開催年:	2006.01.09-2009.01.12

類似資料:

1 テクニカルペーパー Experimental and Computational Investigation of Combustor Acoustics and Instabilities, Part I: Longitudinal Modes R. Smith, N. Nugent, J. Sisco, G. Xia, V. Sankaran, W. Anderson, C. Merkle American Institute of Aeronautics and Astronautics	7 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
2 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	8 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
3 テクニカルペーパー Computational Modeling of Instabilities in a Single-Element Rocket Combustor Using a Response Function R. Smith, G. Xia, W. Anderson, C. Merkle, V. Sankaran American Institute of Aeronautics and Astronautics	9 テクニカルペーパー Impinging jet flow structure and its impact on combustion instability Santoro, R.J., Woodward, R., Schmidt, J., Johnson, D., Yeralan, S., Pal, S., Anderson, W.E. American Institute of Aeronautics and Astronautics
4 テクニカルペーパー Computational Simulations of the Effect of Chamber Diameter on Single-Element Rocket Combustor Instability G. Xia, R. Smith, W. Anderson, C. Merkle American Institute of Aeronautics and Astronautics	10 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
5 テクニカルペーパー Acoustic Mode Simulations in Experimental Rocket Combustors Ellis, M., Xia, G., Sankaran, V., Anderson, W., Merkle, C. American Institute of Aeronautics and Astronautics	11 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
6 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	12 テクニカルペーパー COMPUTATIONAL INSIGHT TO AN EXPERIMENTALLY OBSERVED CHANGE IN THE MIXING CHARACTERISTICS OF AN RBCC ENGINE IN EJECTOR MODE West,J., Ruf,J.H., Cramer,J., Pal,S., Santoro,R. American Institute of Aeronautics and Astronautics

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