DocumentCode
3230951
Title
Whole-field visualisation and velocity measurement of an instantaneous transonic turbine flow
Author
Cross, P. Bryanston ; Udrea, D.D. ; Guenette, G. ; Epstein, A. ; d´Hoop, E.M.
Author_Institution
Dept. of Eng., Warwick Univ., Coventry, UK
fYear
1997
fDate
29 Sep-2 Oct 1997
Firstpage
278
Lastpage
286
Abstract
The work described in this paper represents a premiere in the application of Particle Image Velocimetry (PIV) to turbomachinery flows. This technique allowed the visualisation of the instantaneous transonic flow in the inter-blade passage of a rotating annular cascade at engine conditions. By means of photographic recording of flow tracers and specialised image processing, the instantaneous velocity over the whole field was measured with estimated accuracy between 2 and 5%. Furthermore, the vorticity map was created by means of differentiation and linear interpolation on a Delaunay triangular grid. From the superposition of sequential frames, a steady state velocity map was reconstructed
Keywords
aerospace engines; aerospace testing; flow visualisation; gas turbines; particle velocity analysis; transonic flow; velocity measurement; vortices; Delaunay triangular grid; engine conditions; flow tracers; instantaneous transonic turbine flow; instantaneous velocity; inter-blade passage; linear interpolation; particle image velocimetry; rotating annular cascade; sequential frame superposition; turbomachinery flows; velocity measurement; vorticity map; whole-field visualisation; High speed optical techniques; Image motion analysis; Laboratories; Optical distortion; Optical interferometry; Optical scattering; Optical sensors; Turbines; Velocity measurement; Visualization;
fLanguage
English
Publisher
ieee
Conference_Titel
Instrumentation in Aerospace Simulation Facilities, 1997. ICIASF '97 Record., International Congress on
Conference_Location
Pacific Grove, CA
Print_ISBN
0-7803-4167-8
Type
conf
DOI
10.1109/ICIASF.1997.644690
Filename
644690
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