First Page | Document Content | |
---|---|---|
Date: 2013-05-02 13:43:41Jet 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 AbstractAdd to Reading ListSource URL: www.vsgc.odu.eduDownload Document from Source WebsiteFile Size: 995,24 KBShare Document on Facebook |