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Improved visualization of flow field measurementsA capability was developed that makes it possible to apply to measured flow field data the visualization tools developed to display numerical solutions for computational fluid dynamic problems. The measurement monitor surface (MMS) procedure was applied to the analysis of flow field measurements within a low aspect ratio transonic axial flow fan rotor obtained with 2-D laser anemometry. The procedure generates input for the visualization tools developed to display numerical solutions for computational fluid dynamics problems. The relative Mach number contour plots obtained by this method resemble the conventional contour plots obtained by more traditional methods. The results show that the MMS procedure can be used to generate input for the multidimensional processing and analysis tools developed for data from numerical flow field simulations. They show that an experimenter can apply the MMS procedure to his data and then use an interactive graphics program to display scalar quantities like the Mach number by profiles, carpet plots, contour lines, and surfaces using various colors. Also, flow directionality can be shown by display of vector fields and particle traces.
Document ID
19910009731
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Miles, Jeffrey Hilton
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1991
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-103679
AIAA PAPER 91-0273
E-5896
NAS 1.15:103679
Report Number: NASA-TM-103679
Report Number: AIAA PAPER 91-0273
Report Number: E-5896
Report Number: NAS 1.15:103679
Meeting Information
Meeting: Aerospace Sciences Meeting
Location: Reno, NV
Country: United States
Start Date: January 7, 1991
End Date: January 10, 1991
Sponsors: AIAA
Accession Number
91N19044
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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