Ignition and supersonic combustion behavior of liquid ethanol in a scramjet model combustor with cavity flame holder

Volume: 35, Issue: 2, Pages: 2091 - 2099
Published: Jan 1, 2015
Abstract
null null This study carried out experiments to investigate the combustion behavior of ethanol at Mach 2.0 and stagnation temperatures between 1800 and 2200 K using a supersonic combustor with a cavity flame holder. The distribution of droplet diameters in fuel sprays was measured by a Laser Diffraction Spray Analyzer to estimate the vaporization time of fuel in the combustor. CH chemiluminescences and Schlieren photographs were measured by a...
Paper Details
Title
Ignition and supersonic combustion behavior of liquid ethanol in a scramjet model combustor with cavity flame holder
Published Date
Jan 1, 2015
Volume
35
Issue
2
Pages
2091 - 2099
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