2014
DOI: 10.2322/tjsass.57.101
|View full text |Cite
|
Sign up to set email alerts
|

Application of Two-Photon Absorption Laser-Induced Fluorescence to Atomic Species in the JAXA 750 kW Arc-Heated Wind Tunnel

Abstract: Two-photon absorption laser induced fluorescence (TALIF) is applied to atomic oxygen and nitrogen generated in the JAXA 750 kW arc-heated wind tunnel in order to obtain velocity, translational temperature and atomic number density distributions. Free stream velocity is estimated by Doppler shift and the translational temperature distributions are deduced from spectral broadening. The absolute center excitation wavelength and laser line width are estimated with the TALIF profiles from a static reference cell wh… Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
1

Citation Types

0
1
0

Year Published

2016
2016
2024
2024

Publication Types

Select...
3
1

Relationship

0
4

Authors

Journals

citations
Cited by 4 publications
(1 citation statement)
references
References 21 publications
(17 reference statements)
0
1
0
Order By: Relevance
“…It is well known that a phenolic-based carbon fiber-reinforced phenolic resin composite, referred to as phenolic CFRP herein, has excellent heat resistance and insulation, and is currently used such as a rocket nozzle material of solid rocket and a thermal protection material for re-entry spacecraft. [1][2][3][4][5][6][7][8][9][10][11][12][13][14][15][16][17][18][19][20] It is generally difficult to measure the in-situ temperature of this material in a real application, such as reentry capsules, from the ground. The unknown temperature of the material in such cases may lead to an inefficient design feedback due to the lack of validity of the simulation model relative to the actual usages.…”
Section: Introductionmentioning
confidence: 99%
“…It is well known that a phenolic-based carbon fiber-reinforced phenolic resin composite, referred to as phenolic CFRP herein, has excellent heat resistance and insulation, and is currently used such as a rocket nozzle material of solid rocket and a thermal protection material for re-entry spacecraft. [1][2][3][4][5][6][7][8][9][10][11][12][13][14][15][16][17][18][19][20] It is generally difficult to measure the in-situ temperature of this material in a real application, such as reentry capsules, from the ground. The unknown temperature of the material in such cases may lead to an inefficient design feedback due to the lack of validity of the simulation model relative to the actual usages.…”
Section: Introductionmentioning
confidence: 99%