scholarly journals Erratum: Frequency tripling into the 720–1025‐Å region with pulsed free jets [Rev. Sci. Instrum. 58, 1616 (1987)]

1988 ◽  
Vol 59 (4) ◽  
pp. 673-673
Author(s):  
Ralph H. Page ◽  
Robert J. Larkin ◽  
A. H. Kung ◽  
Y. R. Shen ◽  
Y. T. Lee
Keyword(s):  
Free Jets

Energy Propagation in Heated Turbulent Free Jets

1987 ◽  
Author(s):  
L. Gbahoué ◽  
S. Lecume ◽  
J.L. Carreau ◽  
Ph. Hobbes ◽  
F. Roger
Keyword(s):  
Energy Propagation ◽  
Free Jets

Spray generation from free and half-free jets

2000 ◽  
Author(s):  
T. Sarpkaya ◽  
R. Vaidyanathan
Keyword(s):  
Free Jets

The structure of particle-laden, underexpanded free jets

Shock Waves ◽  
1994 ◽  
Vol 3 (4) ◽  
pp. 299-311 ◽  
Author(s):  
M. Sommerfeld
Keyword(s):  
Free Jets

scholarly journals Scaling law for supersonic core length in circular and elliptic free jets

2021 ◽  
Vol 33 (5) ◽  
pp. 051707
Author(s):  
Arun Kumar Perumal ◽  
Ethirajan Rathakrishnan
Keyword(s):  
Scaling Law ◽  
Free Jets ◽  
Core Length ◽  
Supersonic Core Length

An experimental study of underexpanded sonic, coaxial, swirl jets

2004 ◽  
Vol 218 (1) ◽  
pp. 93-103 ◽  
Author(s):  
K-H Lee ◽  
T Setoguchi ◽  
S Matsuo ◽  
H-D Kim
Keyword(s):  
Static Pressure ◽  
Near Field ◽  
Flow Structures ◽  
Experimental Investigations ◽  
Pressure Measurements ◽  
Annular Nozzle ◽  
Free Jets ◽  
Underexpanded Jets ◽  
Secondary Stream ◽  
The Impact

The present study addresses experimental investigations of the near-field flow structures of an underexpanded sonic, dual, coaxial, swirl jet. The swirl stream is discharged from the secondary annular nozzle and the primary inner nozzle provides the underexpanded free jets. The interactions between the secondary swirl and primary underexpanded jets are quantified by a fine pitot impact and static pressure measurements and are visualized using a shadowgraph optical method. The pressure ratios of the secondary swirl and primary underexpanded jets are varied below 7.0. Experiments are conducted to investigate the effects of the secondary swirl stream on the primary underexpanded jets, compared with the secondary stream of no swirl. The results show that the presence of an annular swirl stream causes the Mach disc to move further downstream, with an increased diameter, and remarkably reduces the fluctuations of the impact pressures in the underexpanded sonic dual coaxial jet, compared with the case of the secondary annular stream with no swirl.

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