Unsteady Nature of Flow Separation Inside a Thrust Optimized Parabolic Nozzle

Unsteady Nature of Flow Separation Inside a Thrust Optimized Parabolic Nozzle

著者名:

掲載資料名:

AIAA paper

シリーズ名:

AIAA Paper : Aerospace Sciences Meeting and Exhibit

シリーズ巻号:

2003

発行年:

2003

通号:

2003-1139

ペーパー番号:

2003-1139

総ページ数:

8

出版情報:

American Institute of Aeronautics and Astronautics

ISSN:

01463705

言語:

英語

請求記号:

A07400

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00001712
シリーズID:	PA00000138
会議名:	AIAA Aerospace Sciences Meeting and Exhibit
回次:	41st
会議開催地:	Reno, NV
会議開催年:	2003.01.06-2003.01.09
論文注記:	41st AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, 6-9 January 2003

類似資料:

1 テクニカルペーパー Goertler Vortex Formation During Shut Down Sequence Inside a Thrust Optimized Parabolic (TOP) Rocket Nozzle Verma, S., Haidn, O. American Institute of Aeronautics and Astronautics	7 テクニカルペーパー Investigation of the Spray Behavior of Gelled Jet A-1 Fuels Using an Air Blast and an Impinging Jet Atomizer. Ciezki, H.K., Robers, A., Schneider, G. American Institute of Aeronautics and Astronautics
2 テクニカルペーパー Study of Flow Unsteadiness in a Hypersonic SWBLI Flowfield on a HAC Model Verma,S.B., Koppenwallner,G. American Institute of Aeronautics and Astronautics	8 テクニカルペーパー Characteristic Flow and Spray Properties of Gelled Fuels with Regard to the Impinging Jet Injector Type J. von Kampen, K. Madlener, H. Ciezki, P. Lozano, S. Sümer American Institute of Aeronautics and Astronautics
3 テクニカルペーパー Investigation of gaseous and solid reaction products in a step combustor using a water-cooled sampling probe Ciezki, H.K., Schwein, B. American Institute of Aeronautics and Astronautics	9 テクニカルペーパー Flow Separation inside a Supersonic Nozzle Exhausting into a Subsonic Compressible Crossflow. Beresh, S.J., henfling, J.F., Erven, R.J. American Institute of Aeronautics and Astronautics
4 テクニカルペーパー Flow Separation Studies in a Subscale Truncated Ideal Contour Nozzle S. Verma, O. Haidn American Institute of Aeronautics and Astronautics	10 テクニカルペーパー Study on Restricted Shock Separation Phenomena in Rocket Nozzles S. Verma, O. Haidn American Institute of Aeronautics and Astronautics
5 テクニカルペーパー Computational Study of Fluidic Thrust Vectoring Using Separation Control in a Nozzle Deere, K., Berrier, B., Flamm, J., Johnson, S. American Institute of Aeronautics and Astronautics	11 テクニカルペーパー LE-7A Engine Nozzle Flow Separation Phenomenon and the Possibility of RSS Suppression by the Step Inside the Nozzle Watanabe, Y., Sakazume, N., Yonezawa, K., Tsujimoto, Y. American Institute of Aeronautics and Astronautics
6 テクニカルペーパー Experimental Investigation of the Acoustics of an Annular Aerospike Nozzle Flow Karthikeyan, N, Verma, S B, Venkatakrishnan, L American Institute of Aeronautics and Astronautics	12 テクニカルペーパー Application of advanced experimental techniques in the development of a cooled turbine nozzle Moon, H.K., Glezer, B. The American Society of Mechanical Engineers

1

2

3

4

5

6

7

8

9

10

11

12