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![]() Date: 2007-09-17 12:10:26Dynamics Scramjet Combustor Shock wave Ramjet Mach number Pressure measurement Rayleigh flow Unstart Jet engines Aerospace engineering Fluid dynamics | Add to Reading List |
![]() | Microsoft Word - VSGC_conf13_paper_draft5DocID: 1rqqS - View Document |
![]() | Characterization of a Dual-Mode Scramjet Combustor via Stereoscopic Particle Image Velocimetry Author: Brian Rice Advisor: Chris Goyne and Jim McDaniel University of Virginia AbstractDocID: 1pDxn - View Document |
![]() | Joint SuperSonic Cruise Missile (JSSCM) ACTD Breakfast Club Brief Capt James Hart N780C/DDocID: 1poZ1 - View Document |
![]() | REDUCTION OF TRIBOELECTRIC CHARGING OF WINDOWS DURING PIV TESTING Meghan R. Luff Advisor: Prof. Christopher P. Goyne The University of Virginia, Charlottesville, VA, 22904 AbstractDocID: 1phnS - View Document |
![]() | High Speed Key Technologies for future Air Transport Research and Innovation Cooperation Scheme HIKARI: Paving the Way towardsDocID: 1o3Fg - View Document |