VMFL032

VMFL032
Turbulent Flow with Separation Along an Axisymmetric Afterbody

Overview

Reference

T.T. Huang, N.C. Groves, “Propeller/stern boundary layer interaction on axisymmetric bodies: Theory and experiment”. David W. Taylor Naval Ship Research and Development Center Report. 76-0113. 1976.

SolverAnsys Fluent, Ansys CFX
Physics/ModelsTurbulent flow
Input File
axiaft.cas for Ansys Fluent
VMFL032B_afterbody.def for Ansys CFX
Project FilesLink to Project Files Download Page

Test Case

Flow past an axisymmetric afterbody, representing the hull of ship. The flow separates on the rear face of the body.

Figure 83: Flow Domain

Flow Domain

Material PropertiesGeometry Boundary Conditions

Density: 1 kg/m3

Viscosity: 1 X 10–6 kg/m-s

Length of the afterbody = 1.0 m

Maximum radius of the afterbody = 0.04556 m

Fully developed turbulent velocity profile on the inlet normal to axis

Axial velocity = 5.9 m/s on the inlet parallel to axis

Analysis Assumptions and Modeling Notes

The far-field boundary of the domain is set parallel to the axis and is modeled as velocity inlet. Fully developed profile is specified at the transverse velocity inlet.

Results Comparison for Ansys Fluent

Figure 84: Comparison of Pressure Coefficient Along the Afterbody Wall

Comparison of Pressure Coefficient Along the Afterbody Wall

Figure 85: Comparison of Skin Friction Coefficient Along the Afterbody Wall

Comparison of Skin Friction Coefficient Along the Afterbody Wall

Results Comparison for Ansys CFX

Figure 86: Comparison of Pressure Coefficient Along the Afterbody Wall

Comparison of Pressure Coefficient Along the Afterbody Wall

Figure 87: Comparison of Skin Friction Coefficient Along the Afterbody Wall

Comparison of Skin Friction Coefficient Along the Afterbody Wall