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Acetone laser induced fluorescence for low pressure/low temperature flow visualization

dc.contributor.authorDonbar, Jeffrey M.en_US
dc.contributor.authorDriscoll, James F.en_US
dc.contributor.authorBryant, R. A.en_US
dc.date.accessioned2006-09-08T20:03:07Z
dc.date.available2006-09-08T20:03:07Z
dc.date.issued2000-05en_US
dc.identifier.citationBryant, R. A.; Donbar, J. M.; Driscoll, J. F.; (2000). "Acetone laser induced fluorescence for low pressure/low temperature flow visualization." Experiments in Fluids 28(5): 471-476. <http://hdl.handle.net/2027.42/42176>en_US
dc.identifier.issn0723-4864en_US
dc.identifier.urihttps://hdl.handle.net/2027.42/42176
dc.description.abstractAcetone fluorescence provides a useful way to visualize the fluid mixing process within supersonic wind tunnels, some of which operate in the low temperature (240–300 K) and low pressure range (0.1–1 atm). Measurements are presented to quantify the dependence of the acetone laser induced fluorescence (LIF) signal on temperature and pressure in this range. The temperature and pressure sensitivity of the acetone LIF signal resulted in less than an 8% variation over the experimental conditions for a laser excitation wavelength of 266 nm. Condensation of the acetone vapor was identified as a potential problem for this diagnostic technique. Methods to prevent and check for condensation are discussed.en_US
dc.format.extent270647 bytes
dc.format.extent3115 bytes
dc.format.mimetypeapplication/pdf
dc.format.mimetypetext/plain
dc.language.isoen_US
dc.publisherSpringer-Verlag; Springer-Verlag Berlin Heidelbergen_US
dc.subject.otherLegacyen_US
dc.titleAcetone laser induced fluorescence for low pressure/low temperature flow visualizationen_US
dc.typeArticleen_US
dc.subject.hlbsecondlevelPhysicsen_US
dc.subject.hlbtoplevelScienceen_US
dc.description.peerreviewedPeer Revieweden_US
dc.contributor.affiliationumDepartment of Aerospace Engineering University of Michigan Ann Arbor, MI 48109-2118, USen_US
dc.contributor.affiliationumDepartment of Aerospace Engineering University of Michigan Ann Arbor, MI 48109-2118, USen_US
dc.contributor.affiliationumDepartment of Aerospace Engineering University of Michigan Ann Arbor, MI 48109-2118, USen_US
dc.contributor.affiliationumcampusAnn Arboren_US
dc.description.bitstreamurlhttp://deepblue.lib.umich.edu/bitstream/2027.42/42176/1/348-28-5-471_00280471.pdfen_US
dc.identifier.doihttp://dx.doi.org/10.1007/s003480050407en_US
dc.identifier.sourceExperiments in Fluidsen_US
dc.owningcollnameInterdisciplinary and Peer-Reviewed


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