Survey of Plasmas Generated in a Mach 5 Wind Tunnel

Survey of Plasmas Generated in a Mach 5 Wind Tunnel

Author(s):

Publication title:

AIAA paper

Title of ser.:

AIAA Paper : Aerospace Sciences Meeting and Exhibit

Ser. no.:

2003

Pub. Year:

2003

No.:

2003-1194

Paper no.:

2003-1194

Pages:

11

Pub. info.:

American Institute of Aeronautics and Astronautics

ISSN:

01463705

Language:

English

Call no.:

A07400

Type:

Technical Paper

Details

TDL ID:	ZA00001712
Series ID:	PA00000138
Conf. info. (Name):	AIAA Aerospace Sciences Meeting and Exhibit
Conf. info. (Number):	41st
Conf. info. (Venue):	Reno, NV
Conf. info. (Date):	2003.01.06-2003.01.09
Note for article:	41st AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, 6-9 January 2003

Similar Items:

1 Technical Paper Effects of Magnetic Fields on Plasma Generated in a Mach 5 Wind Tunnel Menart, J., Shang, J., Kimmel, R., Hayes, J. American Institute of Aeronautics and Astronautics	7 Technical Paper Effect of Magnetic Fields on Surface Plasma Discharges at Mach 5 Kimmel, R., Hayes, J., Menart, J., Shang, J. American Institute of Aeronautics and Astronautics
2 Technical Paper DC Plasma Discharge Effects on a Mach 5 Flow Between Small Plate Electrodes Menart, J., Henderson, S., Shang, J., Kimmel, R., Hayes, J. American Institute of Aeronautics and Astronautics	8 Technical Paper Data Reduction Analysis for a Cylindrical, Double Langmuir Probe Operating in a High Speed Flow Henderson, S., Menart, J., Shang,J., Kimmel, R., Hayes,J. American Institute of Aeronautics and Astronautics
3 Technical Paper Study of Plasma Electrode Arrangements for Optimum Lift in a Mach 5 Flow J. Menart, S. Stanfield, J. Shang, R. Kimmel, J. Hayes American Institute of Aeronautics and Astronautics	9 Technical Paper Application of a Spectroscopic Measuring Technique to Plasma Discharge in Hypersonic Flow S. Stanfield, J. Menart, J. Shang, R. Kimmel, J. Hayes American Institute of Aeronautics and Astronautics
4 Technical Paper Study of Surface and Volumetric Heating Effects in a Mach 5 Flow Menart, J., Henderson, S., Shang, J., Kimmel, R., Hayes, J., Atzbach, C. American Institute of Aeronautics and Astronautics	10 Technical Paper Plasma Actuator for Hypersonic Flow Control Shang, J., Kimmel, R., Menart, J., Hayes, J. American Institute of Aeronautics and Astronautics
5 Technical Paper Technique for Making Microwave Absorption Measurements in a Small Plasma Discharge Kurpik, A., Menart, J., Shang, J., Kimmel, R., Hayes, J. American Institute of Aeronautics and Astronautics	11 Technical Paper Hypersonic Inlet with Plasma Induced Compression J. Shang, J. Menart, R. Kimmel, J. Hayes American Institute of Aeronautics and Astronautics
6 Technical Paper Effect of Surface Plasma Discharges on Boundary Layers at Mach 5 Kimmel, R., Hayes,J., Menart, J., Shang,J. American Institute of Aeronautics and Astronautics	12 Technical Paper Application of Plasma Discharge Arrays to High-Speed Flow Control Kimmel, R., Hayes, J., Menart, J., Shang, J. American Institute of Aeronautics and Astronautics

1

2

3

4

5

6

7

8

9

10

11

12