Inertia and expansion level impact on flow development at various duct sections

Author(s):  
MashtaqAhamed Attar .M ◽  
Ridwan ◽  
Hamza Afser Delvi ◽  
Suheel J. I ◽  
Sher Afghan Khan ◽  
...  
Author(s):  
Mohammed Faheem ◽  
Ridwan ◽  
Rayid Muneer ◽  
Mohammed Aneeque ◽  
Sher Afghan Khan

2019 ◽  
Vol 8 (2S8) ◽  
pp. 1763-1768

This paper presents an experimental study of suddenly expanded flows at supersonic speed is performed. A Convergent-divergent (C-D) nozzle is used with suddenly expanded duct. At the recirculation zone, the pressure is controlled by using four microjets of 1 mm diameter arranged at PCD of 1.3 as an active control mechanism to regulate the pressure in the wake region. The development and the quality of the flow were monitored to ensure that the flow control does not aggravate the flow field in the duct. The geometrical and the inertia parameters are the area ratio and the Mach number. The area of the study was 3.24, L/D ratio was from 10 to 1, and the level of inertia as 2.1. The expansion level considered during the experiments was from 3 to 11. The results clearly indicate that the wall pressure variation with and without control in the enlarged duct does not vary, which means that the use of control does not affect the flow filed in the circular duct.


Water ◽  
2021 ◽  
Vol 13 (13) ◽  
pp. 1718
Author(s):  
Hasan Zobeyer ◽  
Abul B. M. Baki ◽  
Saika Nowshin Nowrin

The flow hydrodynamics around a single cylinder differ significantly from the flow fields around two cylinders in a tandem or side-by-side arrangement. In this study, the experimental results on the mean and turbulence characteristics of flow generated by a pair of cylinders placed in tandem in an open-channel flume are presented. An acoustic Doppler velocimeter (ADV) was used to measure the instantaneous three-dimensional velocity components. This study investigated the effect of cylinder spacing at 3D, 6D, and 9D (center to center) distances on the mean and turbulent flow profiles and the distribution of near-bed shear stress behind the tandem cylinders in the plane of symmetry, where D is the cylinder diameter. The results revealed that the downstream cylinder influenced the flow development between cylinders (i.e., midstream) with 3D, 6D, and 9D spacing. However, the downstream cylinder controlled the flow recirculation length midstream for the 3D distance and showed zero interruption in the 6D and 9D distances. The peak of the turbulent metrics generally occurred near the end of the recirculation zone in all scenarios.


Author(s):  
Mohammed Faheem ◽  
Rayid Muneer ◽  
Mohammed Avvad ◽  
Mohammed Aneeque ◽  
Sher Afghan Khan

1992 ◽  
Vol 28 (1) ◽  
pp. 186-189 ◽  
Author(s):  
V.I. Deev ◽  
V.S. Kharitonov ◽  
V.V. Shako ◽  
A.I. Ageyev ◽  
S.R. Bakhuliev ◽  
...  

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