DocumentCode
273998
Title
A holographic system for aerodynamic testing
Author
Bryanston-Cross, P.J. ; Towers, D.P.
Author_Institution
Warwick Univ., Coventry, UK
fYear
1989
fDate
11-13 Sep 1989
Firstpage
6
Lastpage
15
Abstract
The authors investigate the suitability of holography as an optical flow diagnostic for turbofan nozzle flow structures. In this case a static 1/25th scale model of a powered turbo-fan nacelle has used for nacelle/wing integration studies and evaluated using a holographic technique. The holograms made show the core jet and the by-pass flow as it emerges from the nacelle nozzle system. They also show evidence of structural vibration at the by-pass nozzle wall. A comparison has also been made with alternative non-invasive diagnostic techniques
Keywords
aerospace engines; aerospace testing; flow visualisation; holography; jets; nozzles; vibrations; aerodynamic testing; aerospace testing; by-pass flow; by-pass nozzle wall; core jet; holography; noninvasive diagnostics; optical flow diagnostic; powered turbo-fan nacelle; structural vibration; turbofan nozzle flow structures;
fLanguage
English
Publisher
iet
Conference_Titel
Holographic Systems, Components and Applications, 1989., Second International Conference on
Conference_Location
Bath
Type
conf
Filename
51782
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