<--- Back to Details
First PageDocument Content
Fluid dynamics / Aerodynamics / Compressors / Gas turbine / Marine propulsion / Thermodynamics / Aircraft engine / Combustor / Turbine / Jet engines / Mechanical engineering / Fluid mechanics
Date: 2013-12-11 15:08:05
Fluid dynamics
Aerodynamics
Compressors
Gas turbine
Marine propulsion
Thermodynamics
Aircraft engine
Combustor
Turbine
Jet engines
Mechanical engineering
Fluid mechanics

18th SYMPOSIUM ON INDUSTRIAL APPLICATIONS OF GAS TURBINES

Add to Reading List

Source URL: www.iagtcommittee.com

Download Document from Source Website

File Size: 840,80 KB

Share Document on Facebook

Similar Documents

High-Temperature and Hostile Environment Sensing Through Stress-Wave Propagation Christopher Larsen, Richard A. Roth, and Stuart Shelley Key words: pressure sensor, accelerometer, high-temperature, combustor, remote sens

DocID: 1vj2s - View Document

EFFECTS OF NON CONVENTIONAL LIQUID FUELS FEEDING IN A BUBBLING FLUIDIZED BED COMBUSTOR

DocID: 1v6ld - 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 The following research paper presen

DocID: 1rveQ - View Document

Jet engines / Internal combustion engine / Spaceflight / Spacecraft propulsion / Propulsion / Single-stage-to-orbit / Fluid dynamics / Aircraft engines / Scramjet / Combustor / Ramjet / Particle image velocimetry

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