An Experimental Study of Unsteady Separated Shock Wave / Boundary Layer Interactions

An Experimental Study of Unsteady Separated Shock Wave / Boundary Layer Interactions

著者名:

P. Bruce ( University of Cambridge, Cambridge, Great Britain )
H. Babinsky

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:

2007-1140

ペーパー番号:

AIAA Paper 2007-1140

出版情報:

Reston, Va.: American Institute of Aeronautics and Astronautics

ISSN:

10877215

言語:

英語

請求記号:

A07400/200701 [CD-ROM 2007 Disc 1]

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00050739
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 Unsteady Normal Shock Wave Boundary Layer Interactions with Control P. Bruce, H. Babinsky American Institute of Aeronautics and Astronautics	7 テクニカルペーパー Improving the Lag Entrainment Method in the Case of Transonic Shock Wave/Boundary Layer Interaction Bhanderi, H., Babinsky, H. American Institute of Aeronautics and Astronautics
2 テクニカルペーパー Behaviour of unsteady transonic shock / boundary layer interactions with three-dimensional effects P. Bruce, H. Babinsky American Institute of Aeronautics and Astronautics	8 テクニカルペーパー Experimental Investigation of 3D Shock / Boundary Layer Interaction Control in Transonic Flows H. Ogawa, H. Babinsky American Institute of Aeronautics and Astronautics
3 テクニカルペーパー Experimental Study Of Unsteady Effects in Shock Wave / Turbulent Boundary Layer Interaction P. Polivanov, A. Sidorenko, A. Maslov American Institute of Aeronautics and Astronautics	9 テクニカルペーパー Vortex Generators near Shock/ Boundary Layer Interactions Holden, H., Babinsky, H. American Institute of Aeronautics and Astronautics
4 テクニカルペーパー The Effect of Surface Roughness on Shock Wave/Turbulent Boundary Layer Interactions Babinsky,H., Inger,G. American Institute of Aeronautics and Astronautics	10 テクニカルペーパー Control of Normal Shock Wave/ Turbulent Boundary Layer Interactions Using Streamwise Grooves. Smith, A.N., Holden, H.A., Babinsky, H., Fulker, J.L., Ashill, P.R. American Institute of Aeronautics and Astronautics
5 テクニカルペーパー Improved Boundary Layer Quantities in the Shock Wave Boundary Layer Interaction Region on Bumps Bhanderi, H., Babinsky, H. American Institute of Aeronautics and Astronautics	11 テクニカルペーパー Control of Normal Shock Wave/Turbulent Boundary-Layer Interaction Using Streamwise Slots Smith,A.N., Babinsky,H., Fulker,J.L., Ashill,P.A. American Institute of Aeronautics and Astronautics
6 テクニカルペーパー Micro-Ramp Control for Oblique Shock Wave / Boundary Layer Interactions C. Pitt Ford, H. Babinsky American Institute of Aeronautics and Astronautics	12 テクニカルペーパー Experimental Studies of Laminar Separated Flows Induced by Shock Wave/Boundary Layer and Shock/Shock Interaction in in Hypersonic Flows for CFD Validation Holden, Michael American Institute of Aeronautics and Astronautics

1

2

3

4

5

6

7

8

9

10

11

12