"NASA Technical Reports Server (NTRS) 20170006078: High-Spatial-Resolution OH PLIF Visualization In A Cavity-Stabilized Ethylene-Air Turbulent Flame" - Information and Links:

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"NASA Technical Reports Server (NTRS) 20170006078: High-Spatial-Resolution OH PLIF Visualization In A Cavity-Stabilized Ethylene-Air Turbulent Flame" and the language of the book is English.


“NASA Technical Reports Server (NTRS) 20170006078: High-Spatial-Resolution OH PLIF Visualization In A Cavity-Stabilized Ethylene-Air Turbulent Flame” Metadata:

  • Title: ➤  NASA Technical Reports Server (NTRS) 20170006078: High-Spatial-Resolution OH PLIF Visualization In A Cavity-Stabilized Ethylene-Air Turbulent Flame
  • Author: ➤  
  • Language: English

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  • Internet Archive ID: NASA_NTRS_Archive_20170006078

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"NASA Technical Reports Server (NTRS) 20170006078: High-Spatial-Resolution OH PLIF Visualization In A Cavity-Stabilized Ethylene-Air Turbulent Flame" Description:

The Internet Archive:

High-spatial-resolution OH planar laser-induced fluorescence was measured for a premixed ethylene-air turbulent flame in an electrically-heated Mach 2 continuous-flow facility (University of Virginia Supersonic Combustion Facility, Configuration E.) The facility comprised a Mach 2 nozzle, an isolator with flush-wall fuel injectors, a combustor with optical access, and an extender. The flame was anchored at a cavity flameholder with a backward-facing step of height 9 mm. The temperature-insensitive Q1(8) transition of OH was excited using laser light of wavelength 283.55 nm. A spatial filter was used to create a laser sheet approximately 25 microns thick based on full-width at half maximum (FWHM). Extension tubes increased the magnification of an intensified camera system, achieving in-plane resolution of 40 microns based on a 50% modulation transfer function (MTF). The facility was tested with total temperature 1200 K, total pressure 300 kPa, local fuel/air equivalence ratios of approximately 0.4, and local Mach number of approximately 0.73 in the combustor. A test case with reduced total temperature and another with reduced equivalence ratio were also tested. PLIF images were acquired along a streamwise plane bisecting the cavity flameholder, from the backward facing step to 120 mm downstream of the step. The smallest observed features in the flow had width of approximately 110 microns. Flame surface density was calculated for OH PLIF images.

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  • Added Date: 2022-06-27 05:38:54
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