CFD Predictions of Resistance and Propulsion forthe JAPAN Bulk Carrier (JBC) with and withoutan Energy Saving Device

KADIR BURAK KORKMAZ

Abstract:
Resistance and propulsion predictions for a ship is one of the most important tasks
at the design stage in order to ensure that the ship can sail at a desired speed with
the installed engine capacity and fulfill the mandatory regulations imposed by IMO
such as Energy Efficiency Design Index (EEDI). Since new concerns on environment
and efficiency have risen, predictions are getting more important and as a result
the interests on Energy Saving Device (ESD) increased significantly. Traditional
prediction tools can provide reliable results for resistance and propulsion but it is
time-consuming, expensive and most importantly, scaling problems cannot be eliminated. Since Reynolds similarity is not fulfilled at model test, flow characteristics in
experiments differ significantly from full scale. On the other hand, Computational
Fluid Dynamics (CFD) solves this problem by offering both model and full scale results with a great detail of flow fields. Nevertheless accuracy of CFD is still limited
and accuracy obtained from computations is always a concern.
In this thesis, resistance, sinkage & trim, self-propulsion characteristics and local
flow around the stern are predicted for the new test case JAPAN Bulk Carrier (JBC)
for the Japan 2015 Workshop on CFD in Ship Hydrodynamics. Local flow is examined through mean velocity components, turbulent kinetic energy and Q-criterion
at the stern region. Also, a comprehensive study is performed for revealing the best
settings and procedures for POW tests and self propulsion tests using SHIPFLOW
code. Free surface wave elevation, sinkage & trim are computed with the potential flow solver, viscous flow is evaluated by the Reynolds Averaged Navier-Stokes
(RANS) solver. Propeller simulation is calculated through lifting line based propeller analysis module (LL) of SHIPFLOW. Additionally, a Verification and Validation (V&V) procedure is applied to the resistance, POW and self-propulsion results
in order to assess the uncertainties and numerical errors.