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Method for measuring temperatures and densities in hypersonic wind tunnel air flows using laser-induced O(2) fluorescence.

作者信息

Laufer G, McKenzie R L, Fletcher D G

出版信息

Appl Opt. 1990 Nov 20;29(33):4873-83. doi: 10.1364/AO.29.004873.

DOI:10.1364/AO.29.004873
PMID:20577481
Abstract

Laser-induced fluorescence in oxygen, in combination with Raman scattering, is shown to be an accurate means by which temperature, density, and their fluctuations owing to turbulence can be measured in air flows associated with high speed wind tunnels. For temperatures above 60 K and densities above 0.01 amagat, the uncertainties in the temperature and density measurements can be <2%, if the signal uncertainties are dominated by photon statistical noise. The measurements are unaffected by collisional quenching and can be achieved with laser fluences for which nonlinear effects are insignificant. Temperature measurements using laser-induced fluorescence alone have been demonstrated at known densities in the range of low temperatures and densities which are expected in a hypersonic wind tunnel.

摘要

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