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Flow visualization and interpretation of visualization data for deflected thrust V/STOL nozzlesFlow visualization studies were made for four deflected thrust nozzle models at subsonic speeds. Based on topological rules and the assumption that observed streaks constitute continuous vector fields, available visualization pictures are interpreted and flow patterns on interior surfaces of the nozzles are synthesized. In particular, three dimensional flow structure and separations are discussed. From the synthesized patterns, the overall features of the flow field in a given nozzle can be approximately perceived.
Document ID
19840006079
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kao, H. C.
(NASA Lewis Research Center Cleveland, OH, United States)
Burstadt, P. L.
(NASA Lewis Research Center Cleveland, OH, United States)
Johns, A. L.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1984
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NAS 1.15:83554
NASA-TM-83554
E-1933
Meeting Information
Meeting: Aerospace Sci. Meeting
Location: Reno, NV
Country: United States
Start Date: January 9, 1984
End Date: January 12, 1984
Sponsors: AIAA
Accession Number
84N14147
Funding Number(s)
PROJECT: RTOP 505-40-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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