dc.contributor.author |
Meyers, BC
|
|
dc.contributor.author |
Snedden, Glen C
|
|
dc.contributor.author |
Meyers, Bronwyn C
|
|
dc.contributor.author |
Roos, TH
|
|
dc.contributor.author |
Mahmood, GI
|
|
dc.date.accessioned |
2011-11-15T09:33:57Z |
|
dc.date.available |
2011-11-15T09:33:57Z |
|
dc.date.issued |
2009-09 |
|
dc.identifier.citation |
Meyers, BC, Snedden, GC, Meyer, JP et.al. 2009. Three-dimensional particle image velocimetry in a generic can-type gas turbine combustor. 19th Conference of the International Society for Air Breathing Engines, Montreal, Quebec, Canada, 7-11 September 2009 |
en_US |
dc.identifier.isbn |
9781600867361 |
|
dc.identifier.uri |
http://hdl.handle.net/10204/5288
|
|
dc.description |
19th Conference of the International Society for Air Breathing Engines, Montreal, Quebec, Canada, 7-11 September 2009 |
en_US |
dc.description.abstract |
The three-dimensional flow field inside a generic can-type, forward flow, experimental combustor was measured. A stereoscopic Particle Image Velocimetry (PIV) system was used to obtain the flow field of the combustor in the non-reacting condition. In order for these measurements to be taken, an optically accessible combustor was manufactured. Contour maps of the velocity magnitude is shown which indicates the jet penetration depths while the streamlines show the recirculation zones and flow paths taken by the bulk flow from all inlets to the exit plane. Velocity vectors show the swirling action and the three-dimensional nature of the flow inside a combustor. This data can be used effectively as a test case for Computational Fluid Dynamics (CFD) studies due to the presence of all the flow features of the combustor. |
en_US |
dc.language.iso |
en |
en_US |
dc.publisher |
American Institute of Aeronautics and Astronautics |
en_US |
dc.subject |
Particle Image Velocimetry |
en_US |
dc.subject |
Gas turbine combustor |
en_US |
dc.subject |
PIV |
en_US |
dc.subject |
Flowfield |
en_US |
dc.subject |
Air breathing engines |
en_US |
dc.subject |
Aeronautics |
en_US |
dc.subject |
Astronautics |
en_US |
dc.title |
Three-dimensional particle image velocimetry in a generic can-type gas turbine combustor |
en_US |
dc.type |
Conference Presentation |
en_US |
dc.identifier.apacitation |
Meyers, B., Snedden, G. C., Meyers, B. C., Roos, T., & Mahmood, G. (2009). Three-dimensional particle image velocimetry in a generic can-type gas turbine combustor. American Institute of Aeronautics and Astronautics. http://hdl.handle.net/10204/5288 |
en_ZA |
dc.identifier.chicagocitation |
Meyers, BC, Glen C Snedden, Bronwyn C Meyers, TH Roos, and GI Mahmood. "Three-dimensional particle image velocimetry in a generic can-type gas turbine combustor." (2009): http://hdl.handle.net/10204/5288 |
en_ZA |
dc.identifier.vancouvercitation |
Meyers B, Snedden GC, Meyers BC, Roos T, Mahmood G, Three-dimensional particle image velocimetry in a generic can-type gas turbine combustor; American Institute of Aeronautics and Astronautics; 2009. http://hdl.handle.net/10204/5288 . |
en_ZA |
dc.identifier.ris |
TY - Conference Presentation
AU - Meyers, BC
AU - Snedden, Glen C
AU - Meyers, Bronwyn C
AU - Roos, TH
AU - Mahmood, GI
AB - The three-dimensional flow field inside a generic can-type, forward flow, experimental combustor was measured. A stereoscopic Particle Image Velocimetry (PIV) system was used to obtain the flow field of the combustor in the non-reacting condition. In order for these measurements to be taken, an optically accessible combustor was manufactured. Contour maps of the velocity magnitude is shown which indicates the jet penetration depths while the streamlines show the recirculation zones and flow paths taken by the bulk flow from all inlets to the exit plane. Velocity vectors show the swirling action and the three-dimensional nature of the flow inside a combustor. This data can be used effectively as a test case for Computational Fluid Dynamics (CFD) studies due to the presence of all the flow features of the combustor.
DA - 2009-09
DB - ResearchSpace
DP - CSIR
KW - Particle Image Velocimetry
KW - Gas turbine combustor
KW - PIV
KW - Flowfield
KW - Air breathing engines
KW - Aeronautics
KW - Astronautics
LK - https://researchspace.csir.co.za
PY - 2009
SM - 9781600867361
T1 - Three-dimensional particle image velocimetry in a generic can-type gas turbine combustor
TI - Three-dimensional particle image velocimetry in a generic can-type gas turbine combustor
UR - http://hdl.handle.net/10204/5288
ER -
|
en_ZA |