Experiments in Unsteady Forcing of Mach 2 Shock Wave/Boundary Layer Interactions

Experiments in Unsteady Forcing of Mach 2 Shock Wave/Boundary Layer Interactions

著者名:

P. Bueno ( University of Texas, Austin, TX )

J. Wagner

J. Searcy

B. Ganapathisubramani

N. Clemens

D. Dolling

さらに 1 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:

2006-0878

ペーパー番号:

AIAA Paper 2006-878

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 Cinematographic Planar Imaging of a Mach 2 Shock Wave/Turbulent Boundary Layer Interaction Bueno, P., Clemens, N., Dolling, D., Ganapathisubramani, B. American Institute of Aeronautics and Astronautics	7 テクニカルペーパー The Relationship Between Upstream Turbulent Boundary Layer Velocity Fluctuations and Separation Shock Unsteadiness Beresh, S. J., Clemens, N. T., Dolling, D. S. American Institute of Aeronautics and Astronautics
2 テクニカルペーパー Wide-Field PIV of Pulsed Jet Injection Upstream of Mach 2 Shock Wave/Boundary Layer Interaction Bueno,P., Hou,Y., Clemens, N., Dolling, D. American Institute of Aeronautics and Astronautics	8 テクニカルペーパー Effects of Upstream Coherent Structures on Low-Frequency Motion of Shock-Induced Turbulent Separation B. Ganapathisubramani, N. Clemens, D. Dolling American Institute of Aeronautics and Astronautics
3 テクニカルペーパー Planar imaging measurements to study the effect of spanwise structure of upstream turbulent boundary layer on shock induced separation B. Ganapathisubramani, N. Clemens, D. Dolling American Institute of Aeronautics and Astronautics	9 テクニカルペーパー The relationshop between upstream turbulent boundary layer velocity fluctuations and separation shock unsteadiness Beresh, S.J., Clemens, N.T., Dolling, D.S. American Institute of Aeronautics and Astronautics
4 テクニカルペーパー Experimental Studies of Transitional Boundary Layer Shock Wave Interactions Z. Murphree, J. Jagodzinski, E. Hood, N. Clemens, D. Dolling American Institute of Aeronautics and Astronautics	10 テクニカルペーパー The Effects of Upstream Mass Injection on a Mach 2 Cavity Flow. Bueno, P.C., Unalmis, O.H., Clemens, N.T., Dolling, D.S. American Institute of Aeronautics and Astronautics
5 テクニカルペーパー PIV Investigation of Role of Boundary Layer Velocity Fluctuations in Unsteady Shock-Induced Separation Unalmis, O. H., Hou, Y. X., Bueno, P. C., Clemens, N. T., Dolling, D. S. American Institute of Aeronautics and Astronautics	11 テクニカルペーパー The effects of the incoming turbulent boundary layer structure on a shock-induced separated flow Beresh, S.J., Comninos, M., Clemens, N.T., Dolling, D.S. American Institute of Aeronautics and Astronautics
6 テクニカルペーパー Experimental Studies of Transitional Boundary Layer Shock Wave Interactions Z. Murphree, K. Yuceil, N. Clemens, D. Dolling American Institute of Aeronautics and Astronautics	12 テクニカルペーパー Development of a Multi-Camera PIV Imaging System for Studies of Shock/Boundary Layer Interactions. Hou, Y.X., Clemens, N.T., Dolling, D.S. American Institute of Aeronautics and Astronautics

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