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Jet engines / Fluid dynamics / Spacecraft propulsion / Single-stage-to-orbit / Measurement / Scramjet / Combustor / Hy-V / Ramjet / Flow measurement / Particle image velocimetry / Shock wave
Date: 2013-05-02 13:43:41
Jet engines
Fluid dynamics
Spacecraft propulsion
Single-stage-to-orbit
Measurement
Scramjet
Combustor
Hy-V
Ramjet
Flow measurement
Particle image velocimetry
Shock wave

Characterization of a Dual-Mode Scramjet Combustor via Stereoscopic Particle Image Velocimetry Author: Brian Rice Advisor: Chris Goyne and Jim McDaniel University of Virginia Abstract

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