A study on Numerical Analysis of Controllable Pitch Propeller(CPP) using tunnel inspection AUV

Jung, Hyun-Chul; Kim, Min Jung; Lee, Phil-Yeob; Jung, Hojin

doi:10.1109/oceans-yeosu.2012.6263551

Cited by 1 publication

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“…Chen et al [11], hydro-dynamically analyzed a submersible glider for the role of the glider wing in a nonuniform flow. Jung et al [16] studied the effects of changes in pitch of the propeller and its applications such as backward movement in tunnels. Gao et al [17] studied a numerical model of a glider with two wings on each side that is angled to the body.…”

Section: Introductionmentioning

confidence: 99%

Numerical Simulation of Hydrodynamic Properties of Alex Type Gliders

Divsalar

Shafaghat

Farhadi

et al. 2020

IJE

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This work presents a numerical Simulation of an underwater glider to investigate the effect of angle of attack on the hydrodynamic coefficients such as lift, drag, and torque. Due to the vital role of these coefficients in designing the controllers of a glider, and to obtain an accurate result, this simulation has been carried on at a range of operating velocities. The total length of the underwater glider with two wings is 900 mm with a 4-digits NACA0009 profile. The fluid flow regime is discretized and solved by computational fluid dynamics and finite volume method. Since the Reynolds number range for this study is in a turbulent flow state (up to 3.7e06), the κ-ω SST formulation was used to solve Navier-Stokes equations and continuity and the angles of attack ranging are from-8 to 8 degrees. The main purpose of this research is to study the effect of each of the dynamics parameters of glider motion such as velocity and angle of attacks on the hydrodynamic coefficients. Based on the results, the drag and lift coefficients are enhanced with increasing the angle of attack. In addition, the drag coefficient enhanced with increasing the velocity however, when the glider velocity is increased, the lift coefficient does not change significantly except at the highest angle of attack that decreases. The highest drag coefficient is 0.0246, which corresponds to the angle of attack of-8 and the Reynolds number of 3738184. In addition to simple geometry, the glider studied in this paper shows relatively little resistance to flow.

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Section: Introductionmentioning

confidence: 99%