48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition 2010
DOI: 10.2514/6.2010-856
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Progress on a Rayleigh Scattering Mass Flux Measurement Technique

Abstract: = scattering angle (rad)

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“…Typical frequency drift observed in the Rayleigh work at NASA GRC is 5 -20 MHz, giving velocity errors of 2 -8 m/s. In many Rayleigh scattering experiments utilizing a CCD camera to detect the interference fringe pattern a small amount of incident laser light is spectrally analyzed along with the Rayleigh scattered light to provide a simultaneous reference of the incident laser signal, thereby eliminating the velocity measurement uncertainty attributable to laser frequency drift [11][12][13] . However, when this is done there is often significant overlap of the Rayleigh and reference fringes in the image because the frequency shift between the two signals is not large enough to distinctly separate the two fringes.…”
Section: Introductionmentioning
confidence: 99%
“…Typical frequency drift observed in the Rayleigh work at NASA GRC is 5 -20 MHz, giving velocity errors of 2 -8 m/s. In many Rayleigh scattering experiments utilizing a CCD camera to detect the interference fringe pattern a small amount of incident laser light is spectrally analyzed along with the Rayleigh scattered light to provide a simultaneous reference of the incident laser signal, thereby eliminating the velocity measurement uncertainty attributable to laser frequency drift [11][12][13] . However, when this is done there is often significant overlap of the Rayleigh and reference fringes in the image because the frequency shift between the two signals is not large enough to distinctly separate the two fringes.…”
Section: Introductionmentioning
confidence: 99%