Instantaneous temperature imaging in hypersonic flows using laser-induced fluorescence of high rotational-quantum-number transitions

P. M. Danehy, C. D. Hill, S. O'Byrne, J. S. Fox, A. F.P. Houwing

Research output: Contribution to conferencePaperpeer-review

1 Citation (Scopus)

Abstract

This paper investigates the use of one-line laser-induced fluorescence (LIF) thermometry of nitric oxide to study hypersonic flows generated by free-piston shock tunnels. This method has several advantages including lower cost, simpler set up, and reduced errors from optical thickness compared to two-line LIF thermometry. However, comparisons between one-line and two-line fluorescence thermometry indicate that the method is unreliable in air flows. The method is used to provide qualitative temperature maps in the separated flow region forward of a blunt fin attached to a flat plate in a Mach 6.4 freestream.

Original languageEnglish
DOIs
Publication statusPublished - 2000
Event21st Aerodynamic Measurement Technology and Ground Testing Conference 2000 - Denver, CO, United States
Duration: 19 Jun 200022 Jun 2000

Conference

Conference21st Aerodynamic Measurement Technology and Ground Testing Conference 2000
Country/TerritoryUnited States
CityDenver, CO
Period19/06/0022/06/00

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