Electron density measurement behind a shock wave by means of Hｦﾂ line profile matching

Electron density measurement behind a shock wave by means of Hｦﾂ line profile matching

Author(s):

Fujita, K. ( The Institute of Space & Astronautical Science, Japan )
Abe, T.
Sato, S.
Otsu, T.
Ebinuma, Y.

Publication title:

AIAA paper

Title of ser.:

AIAA Paper : AIAA Thermophysics Conference

Ser. no.:

1999

Pub. Year:

1999

No.:

99-3684

Paper no.:

99-3684

Page(from):

1

Page(to):

9

Pub. info.:

American Institute of Aeronautics and Astronautics

ISSN:

01463705

Language:

English

Call no.:

A07400

Type:

Technical Paper

Details

TDL ID:	ZA00050871
Series ID:	PA00000150
Conf. info. (Name):	AIAA Thermophysics Conference
Conf. info. (Number):	33rd
Conf. info. (Venue):	Norfolk, VA
Conf. info. (Date):	1999.06.28-1999.07.01
Note for article:	33rd Thermophysics Conference, 28 June-1 July, 1999/Norfolk, Va

Similar Items:

1 Technical Paper Electron Density Measurement behind a Shock Wave by Means of Hｦﾂ Line Profile Matching Fujita, K., Abe, T., Sato, S., Otsu, T., Ebinuma, Y. American Institute of Aeronautics and Astronautics	7 Technical Paper Shock Layer enhancement by electro-magnetic effect for spherical blunt body A. Matsuda, K. Wakatsuki, Y. Takizawa, M. Kawamura, H. Otsu, D. Konigorski, S. Sato, T. Abe American Institute of Aeronautics and Astronautics
2 Technical Paper Experimental investigation of air radiation from behind a strong shock wave Fujita, K., Sato, S., Abe, T., Ebinuma, Y. American Institute of Aeronautics and Astronautics	8 Technical Paper Measurements of Rovibrational Temperatures Derived from N₂ (1+) and N₂ (2+) behind Shock Waves G. Yamada, H. Takayanagi, K. Fujita, T. Suzuki American Institute of Aeronautics and Astronautics
3 Technical Paper Electron Temperature and Density Measurement ahead of Strong Shock Waves Fujita,K., Sato,S., Abe,T., Matsuda,A. American Institute of Aeronautics and Astronautics	9 Technical Paper Assessment of the Thermochemical Model for a Super-Orbital Reentry Flow. Otsu, H., Sasoh, A., Fujita, K., Abe, T. American Institute of Aeronautics and Astronautics
4 Technical Paper Translational Temperature Measurement for Atomic Oxygen Behind Shock Waves by Absorption Spectroscopic Technique Fujita, K., Sato, S., Abe, T. American Institute of Aeronautics and Astronautics	10 Technical Paper Interaction between Shock Wave and Glow Discharge Plasmas Sato, E., Sato, S., Abe, T. American Institute of Aeronautics and Astronautics
5 Technical Paper Experimental Study of Nonequilibrium Phenomena Behind Strong Shock Waves Generared in Super-Orbital Reentry Flight. Matsuda, A., Fujita, K., Sato, S., Abe, T. American Institute of Aeronautics and Astronautics	11 Technical Paper Reentry Environment Advanced Diagnostics (READ) Flight Experiment on USERS Reentry Vehicle Abe,T., Fujita,K., Otsu,H., Hama,K., Shingu,S., Ichizono,K. American Institute of Aeronautics and Astronautics
6 Technical Paper State-to-state Nonequilibrium rotational Kinetics of Nitrogen Behind a Strong Shock Wave. Fujita, K., Abe, T. American Institute of Aeronautics and Astronautics	12 Technical Paper Ro-Vibrational Temperatures Derived from N2(2+) Emission Spectra and CARS Method Behind Strong Shock Waves A. Matsuda, M. Ota, S. Batter, K. Arimura, K. Maeno, T. Abe American Institute of Aeronautics and Astronautics

1

2

3

4

5

6

7

8

9

10

11

12