<--- Back to Details
First PageDocument Content
Aerodynamics / Jet engines / Aerospace engineering / Engineering / Spaceflight / Spacecraft propulsion / Fluid dynamics / Airspeed / Shock wave / Scramjet / Hypersonic speed / Ramjet
Date: 2016-03-06 18:36:55
Aerodynamics
Jet engines
Aerospace engineering
Engineering
Spaceflight
Spacecraft propulsion
Fluid dynamics
Airspeed
Shock wave
Scramjet
Hypersonic speed
Ramjet

Mixing Enhancement in Supersonic Combustion Ramjets

Add to Reading List

Source URL: www.ifd.mavt.ethz.ch

Download Document from Source Website

File Size: 1,00 MB

Share Document on Facebook

Similar Documents

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 The following research paper presen

DocID: 1rveQ - View Document

Microsoft Word - VSGC_conf13_paper_draft5

Microsoft Word - VSGC_conf13_paper_draft5

DocID: 1rqqS - View Document

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

DocID: 1qrD8 - View Document

StudentConf agenda-2011-Final.xlsx

StudentConf agenda-2011-Final.xlsx

DocID: 1pVq8 - 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 Abstract

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

DocID: 1pDxn - View Document