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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
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Document Date: 2013-05-02 13:43:32


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