Velocity and NO-Lifetime Measurements in an Unseeded Hypersonic Air Flow
Autores
Journal of Fluids Engineering Transactions of the ASME , vol. 140 , no. 12 , Article 121105
ISSN: 00982202
Resumo
Copyright © 2018 by ASME.A laser-induced fluorescence (LIF)-based nitric-oxide flow-tagging technique was applied to measure both velocity and NO lifetime in a hypersonic shock tunnel from two experimental test runs. The results were supported by an analytical profile proposed in this paper that provides a way to correct velocity measurements under unknown systematic error sources. This procedure provided velocities with discrepancies lower than 3% for a total of five measurements, and lower than 2% when compared with that obtained from a linear fit. Additionally, the comparison between the proposed and experimental profiles allowed us to obtain the fluorescence NO lifetime from only one image.
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