Preliminary Investigation of Thermochemical Nonequilibrium behind a Strong Shock Wave with Precursor Photoionization in Argon

Preliminary Investigation of Thermochemical Nonequilibrium behind a Strong Shock Wave with Precursor Photoionization in Argon

Author(s):

H. Katsurayama ( Japan Aerospace Exploration Agency, Sagamihara, Kanagawa, Japan )
A. Matsuda
T. Abe

Publication title:

AIAA meeting papers on disc

Title of ser.:

AIAA Paper : AIAA Thermophysics Conference

Ser. no.:

2007

Pub. Year:

2007

No.:

2007-4552

Paper no.:

AIAA Paper 2007-4552

Pub. info.:

Reston, Va.: American Institute of Aeronautics and Astronautics

ISSN:

10877215

Language:

English

Call no.:

A07400/200715 [CD-ROM 2007 Disc 15]

Type:

Technical Paper

Details

TDL ID:	ZA00049507
Series ID:	PA00000150
Conf. info. (Name):	AIAA Thermophysics Conference
Conf. info. (Number):	39th
Conf. info. (Venue):	Miami, Florida
Conf. info. (Date):	2007.06.25-2007.06.28
Note for article:	39th AIAA Thermophysics Conference, Miami, Florida, June 25-28, 2007

Similar Items:

1 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	7 Technical Paper Particle Simulation of Electromagnetic Control of a Weakly Ionized Flow past a Blunt Body H. Katsurayama, M. Kawamura, A. Matsuda, T. Abe American Institute of Aeronautics and Astronautics
2 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	8 Technical Paper Radiation Behind the Strong Shock Waves: Experiments and Modeling E. Anohin, T. Ivanova, N. Koudriavtsev, A. Starikovskii American Institute of Aeronautics and Astronautics
3 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	9 Technical Paper Experimental Study on Drag Enhancement in Electrodynamic Heat Shield for a Blunt Body in a Weakly Ionized Plasma Flow M. Kawamura, A. Matsuda, H. Katsurayama, H. Otsu, D. Konigorski, S. Sato, T. Abe American Institute of Aeronautics and Astronautics
4 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	10 Technical Paper Numerical investigation of shock/vortex interaction in hypersonic thermochemical nonequilibrium flow Yamamoto, S., Takasu, N., Nagatomo, H. American Institute of Aeronautics and Astronautics
5 Technical Paper Numerical Simulation of Electromagnetic Flow Control in a One-Kilowatt Class Argon Arcjet WIndtunnel H. Katsurayama, T. Abe American Institute of Aeronautics and Astronautics	11 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
6 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	12 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

1

2

3

4

5

6

7

8

9

10

11

12