TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN
Online ISSN : 1884-0485
ISSN-L : 1884-0485
a) Chemical Propulsion and Air-breathing Engines
Temperature Measurement by Two-Band Emission Method with CO2 and H2O Molecules
Yuki MORIShunya SHIMADAShuhei TAKAHASHITadayoshi IHARAShinji NAKAYAMitsuhiro TSUE
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2016 Volume 14 Issue ists30 Pages Pa_21-Pa_26

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Abstract

Two-band emission method for measuring temperature distribution using CO2 or H2O as the emission medium was developed. In the calibration test using McKenna hydrogen flat flame burner, the developed method had similar quantitativity compared with the other measurement methods, CARS and SiC radiant method. When we applied the developed two-band emission method to high enthalpy supersonic wind tunnel experiment, we could capture the behavior of shockwaves and expansion fans in the supersonic flow and the reconstructed temperature distribution was reasonably quantitative.

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© 2016 The Japan Society for Aeronautical and Space Sciences
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