NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
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. Previously announced in STAR as N84-14147
Document ID
19840039065
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
August 12, 2013
Publication Date
January 1, 1984
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
AIAA PAPER 84-0102
Accession Number
84A21852
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available