Abstract

Defense applications for both under oceans and seas, particularly underwater vehicles have been considered in this research. With this aim, flow characteristics around a torpedo-like geometry under the effect of the boundary layer flow over a smooth flat plate have been experimentally examined by using PIV technique. All of the experiments have been done for Re=20000 and Re=40000 based on the length (L) of the geometry as a characteristic length. As a result, time-averaged streamwise velocity components , velocity vectors , streamline topologies and Reynolds stress correlations in the wake region of the torpedo-like geometry have been acquired in the range of 0 ≤ G/D ≤ 1.5. Here, G is the space between the bottom point of the geometry and flat plate surface; D stands for the diameter of the geometry. It is found that at the smallest value of G/D=0.25, jet-like flow occurs between the plate and the model which causes a powerful scouring. As the gap ratio is increased to G/D=0.5 and G/D=1.0, the jet-like flow diminishes slightly and then the flow structure in the wake region becomes similar to the uniform incoming flow condition for G/D=1.50. Due to the effect of the jet-like flow and boundary layer flow, time-averaged flow patterns present asymmetrical distributions which are clearly shown a bigger size focus close to the plate in streamline topology. Reynolds stress patterns form more powerful viscous forces in the boundary layer flow due to the occurrence of eddy vortices and viscosity effect. It is observed from the aforementioned flow patterns that interaction between the flow structure, the model and boundary layer flow yields very complex structure. In order to decrease the energetic flow in this condition, passive or active flow control method can be integrated on the torpedo-like geometry.

Highlights

  • Torpedoes, torpedo-like geometries and underwater unmanned vehicles have been investigated in this research

  • Ozgoren et al (2013) investigated flow patterns around sphere placed over flat plate by using Particle Image Velocimetry (PIV) and dye visualization

  • The closer position of the sphere to the wall result in distribution of Reynolds stress correlations (u'ν'/U∞2). They found the boundary layer thickness about 63 mm and observed flow characteristics around sphere at different gap ratios with flat plate for 0 ≤ G/D ≤ 1.5 at 2500 ≤ Re ≤ 10000 in terms of the turbulent boundary layer generated by using trip wire

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Summary

Introduction

Torpedo-like geometries and underwater unmanned vehicles have been investigated in this research. Ozgoren et al (2011) have compared the flow structures in the wake region of both a cylinder and a sphere They have done experiments of immersed bodies which were in the free-stream flow for Re=5000 and Re=10000 and they have used PIV and dye techniques. Hajimirzaie et al (2014) examined the mean wake and turbulent flow field around sphere placed structures by using experimental methods which are Particle Image Velocimetry (PIV) and Thermal Anemometry methods, they investigated at Reynolds number of 17800. They examined the flow surrounding the spherical obstacle by PIV techniques, and anemometry measurements used to characterize the instability in the weak. The aim of this study is to examine the flow structures around a torpedo-like geometry placed in a boundary layer flow, experimentally

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