S054042 Flow Characteristics of a Plane Jet with Serrated Tabs at the Nozzle Exit

2013 ◽  
Vol 2013 (0) ◽  
pp. _S054042-1-_S054042-5 ◽  
Author(s):  
Fumiya YOSHIDA ◽  
Takahiro KIWATA ◽  
Taichi USUZAWA ◽  
Wataru HINOMOTO
2016 ◽  
Vol 2016 (0) ◽  
pp. 0223
Author(s):  
Makito SAKAI ◽  
Takahiro KIWATA ◽  
Hiroshi TERAMOTO ◽  
Takumi AWA ◽  
Kuniaki TOYODA

1989 ◽  
Vol 8 (1-2) ◽  
pp. 77-85 ◽  
Author(s):  
G. J. Hitchman ◽  
A. A. Abdel-Rahman ◽  
P. R. Slawson ◽  
A. B. Strong

2012 ◽  
Vol 2012.49 (0) ◽  
pp. 051501-051502
Author(s):  
Taichi USUZAWA ◽  
Wataru HINOMOTO ◽  
Takahiro KIWATA ◽  
Shigeo KIMURA ◽  
Nobuyoshi KOMATSU

2011 ◽  
Vol 2011 (0) ◽  
pp. _S054082-1-_S054082-5
Author(s):  
Wataru HINOMOTO ◽  
Takahiro KIWATA ◽  
Shigeo KIMURA ◽  
Nobuyoshi KOMATSU

1976 ◽  
Vol 98 (3) ◽  
pp. 443-446
Author(s):  
A. K. Stiffler

A turbulent jet is perturbed transverse to the flow direction by periodic pressure gradients near the nozzle exit. Transit velocities are defined in terms of the measured signal time delay for stations 8, 12, 16 nozzle widths downstream of the nozzle exit. Excitation frequencies to 800 cps are considered. Transit velocities are found to be much less than the jet centerline velocity. The results are related to the convection velocity of turbulence.


2010 ◽  
Vol 5 (1) ◽  
pp. 183-199
Author(s):  
Katsuya HIRATA ◽  
Kazuaki SHOBU ◽  
Taisuke MURAYAMA ◽  
Jiro FUNAKI

1986 ◽  
Vol 108 (1) ◽  
pp. 82-88 ◽  
Author(s):  
J. R. R. Pelfrey ◽  
J. A. Liburdy

A detailed study of the mean flow characteristics of a turbulent offset jet is presented. The flow is characterized by a longitudinal variation of curvature, skewed impingement onto a flat surface, a recirculating region, and the development of a wall jet region. Flow structure is described in the preimpingement, recirculation and impingement regions. An interdependence is shown among the pressure differential across the jet, jet curvature and entrainment. The magnitude of the curvature strain rate is found to be significant and implies that this flow cannot be accurately modelled as a thin shear layer. The jet decay and spread rates are similar to those of a plane jet if appropriate curved coordinates are used. The extent of the impingement region is approximately 20 nozzle widths downstream, in agreement with previous studies.


2009 ◽  
Vol 2009.19 (0) ◽  
pp. 420-423
Author(s):  
Taisuke MURAYAMA ◽  
Kazuaki SHOUBU ◽  
Jiro FUNAKI ◽  
Katsuya HIRATA

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