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LDV Measurements in an Annular Combustor Model (in English)
National Aeronautics and Space Administr
(Author)
·
Dean A. Barron
(Author)
·
Biblioscholar
· Paperback
LDV Measurements in an Annular Combustor Model (in English) - National Aeronautics and Space Administr ; Barron, Dean A.
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Synopsis "LDV Measurements in an Annular Combustor Model (in English)"
This thesis covers the design and setup of a laser doppler velocimeter (LDV) system used to take velocity measurements in an annular combustor model. The annular combustor model is of contemporary design using 60 degree flat vane swirlers, producing a strong recirculation zone. Detailed measurements are taken of the swirler inlet air flow and of the downstream enclosed swirling flow. The laser system used is a two color, two component system set up in forward scatter. Detailed are some of the special considerations needed for LDV use in the confined turbulent flow of the combustor model. LDV measurements in a single swirler rig indicated that the flow changes radically in the first duct height. After this, a flow profile is set up and remains constant in shape. The magnitude of the velocities gradually decays due to viscous damping.
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The book is written in English.
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