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Design criteria for and applications of the vortex generator mixing principalThere are at this date numerable projects, in various Divisions of U.A.C., either in progress or contemplated, which are employing the vortex generator mixing principle. This principle is defined as the method which utilises tip vortices generated by low aspect ratio airfoils for the purpose of transverse mixing of the flow of a confined fluid medium where the axis of the vortex is parallel to the direction of flow. To date, vortex generator design criteria have not been published. Therefore, for the assistance of those individuals concerned and in the interest of the vortex mixing principle, the following material (subject to modifications) is presented in this memorandum report.
Document ID
19680068324
Acquisition Source
Langley Research Center
Document Type
Contractor or Grantee Report
Authors
H D Taylor
(United Aircraft Corporation Hartford, Connecticut, United States)
Date Acquired
August 4, 2013
Publication Date
February 16, 1948
Publication Information
Publisher: National Advisory Committee for Aeronautics
Subject Category
Aircraft Design, Testing and Performance
Report/Patent Number
M-15038-1
Report Number: M-15038-1
Accession Number
68N83135
Funding Number(s)
CONTRACT_GRANT: NA
Distribution Limits
Public
Copyright
Public Use Permitted.
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