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contributor authorMatos, Pedro A. de S.
contributor authorBarreta, Luiz G.
contributor authorMartins, Cristiane A.
date accessioned2019-02-28T10:59:51Z
date available2019-02-28T10:59:51Z
date copyright6/26/2018 12:00:00 AM
date issued2018
identifier issn0098-2202
identifier otherfe_140_12_121105.pdf
identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4251555
description abstractA 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.
publisherThe American Society of Mechanical Engineers (ASME)
titleVelocity and NO-Lifetime Measurements in an Unseeded Hypersonic Air Flow
typeJournal Paper
journal volume140
journal issue12
journal titleJournal of Fluids Engineering
identifier doi10.1115/1.4039863
journal fristpage121105
journal lastpage121105-8
treeJournal of Fluids Engineering:;2018:;volume( 140 ):;issue: 012
contenttypeFulltext


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