NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Computational analysis of the flowfield of a two-dimensional ejector nozzleA time-iterative full Navier-Stokes code, PARC, is used to analyze the flowfield of a two-dimensional ejector nozzle system. A parametric study was performed for two controlling parameters, duct to nozzle area ratio and nozzle pressure ratio. Results show that there is an optimum area ratio for the efficient pumping of secondary flow. At high area ratios, a freestream flow passes directly through the mixing duct without giving adequate pumping. At low area ratios, the jet boundary blocks the incoming flow. The nozzle pressure ratio variation shows that the pumping rate increases as the pressure ratio increases, provided there is no interaction between the shroud wall and the shock cell structure.
Document ID
19900055635
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Choi, Y. H.
(NASA Lewis Research Center Cleveland, OH, United States)
Soh, W. Y.
(NASA Lewis Research Center Cleveland, OH; Sverdrup Technology, Inc., Brook Park, OH, United States)
Date Acquired
August 14, 2013
Publication Date
July 1, 1990
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
AIAA PAPER 90-1901
Accession Number
90A42690
Funding Number(s)
CONTRACT_GRANT: NAS3-25266
Distribution Limits
Public
Copyright
Other

Available Downloads

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