A particle image velocimetry (PIV) investigation of a scramjet combustor with a cavity flameholder is described. The first phase of planned research will apply two-dimensional PIV to a measurement plane within the cavity

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Date: 2013-05-02 13:43:32 Measurement Fluid dynamics Jet engines Particle image velocimetry Propulsion Aircraft engines Spacecraft propulsion Spaceflight Velocimetry Combustor Scramjet PIV		A particle image velocimetry (PIV) investigation of a scramjet combustor with a cavity flameholder is described. The first phase of planned research will apply two-dimensional PIV to a measurement plane within the cavity Add to Reading List Source URL: www.vsgc.odu.edu Download Document from Source Website File Size: 12,92 KB Share Document on Facebook

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