The application of CAESES from a perspective of a

The application of CAESES from a perspective of a propeller makerDavid Bendl, 2017-09-28

Voith Propulsion

VOITH CAESES | David Bendl | 2017-09-28 2

VLJ Integration Study

VLJ Propulsion Arrangement

inlet tunnel ShaftVLJoutlet tunnel

Geometry DefinitionIntegration Parameters

VLJ integration depth

Geometry DefinitionRotor and Stator

r/R [-]

• blade parameters are defined on cylinder sections [r/R]

• chord relative to diameter

• thickness, camber, skew, rake relative to chord

• pitch [°] normalized by 90°

• profile is generated on 2D plane (curve engine)

• subsequent block structured grid generation requires support geometry

• circle segment shows cylinder section for final profile position

• profile for three positions is shown (r/R = 0.4, 0.7, 1.0)

• view on the three cylinder sections

• based on the profile curve engine the whole blade is created as meta surface

Geometry DefinitionNozzle

• nozzle is a simple rotational body

• rotor and stator are positioned inside of the nozzle

Geometry DefinitionNozzle and Shaft

• shaft and hub complete propulsion line

Geometry DefinitionInlet Tunnel

• the circle’s axis is parallel to the rotor axis

• the circle’ axis defines a plane that intersects the following definition curves and creates three circle points: tunnel apex, side A and side B

• integration requires a inlet tunnel

• curve engine is a three point circle

tunnel apex

side A

side B

Geometry DefinitionInlet Tunnel

• tunnel is created as meta surface

Geometry DefinitionHull

• hull has a generic shape that a simple integration

Geometry DefinitionHull and Inlet Tunnel

• inlet tunnel geometry is combined with hull geometry

• all surfaces are combined to one brep

• no boolean operations are used � more stable

Geometry DefinitionHull and VLJ Assembly

• hull brep and VLJ brep are combine by booleanunion (careful base geometry definition assures success � tolerances)

• outlet tunnel is a simple extrusion of the nozzle’s outlet as a boolean difference

Grid GenerationRotor and Stator (Structured Hexahedron Approach)

• rotor and stator mesh are created by Icem Hexa

• only one blade is meshed, whole rotor is defined rotated copies

• all the support geometry (curves and surfaces) are needed for ...

• ... the block structure of the hexahedron mesh

• circumferential symmetry is assured

• surface mesh has high density in regions of interest: leading edge, trailing edge, gap between nozzle and blade tip

• prism layer around all surfaces

Grid GenerationHull Control Volume (Unstructured Polyhedron Approach)

• around the hull a half pipe control volume is created

• this region discretized by polyhedrons

Grid GenerationHull and Control Volume (Unstructured Polyhedron Approach)

• complete control volume is created by extruding in- and outlet grid

Grid GenerationSurface Mesh

Control VolumeBoundary Definition

velocity inlet

pressure outlet

slip wall

noslip wall(rotational velocity)

Integration StudyIntegration Depth and Shaft Inclination

VIT Hull Interaction Study

VIT Interaction StudyBow Setup

VIT Interaction StudyFlowparts (Tunnel Hull Transition)

flowpart

Geometry DefinitionHull and Flowpart Parameters

Geometry DefinitionBow

• bow geometry is based on simple three point b-spline curves

• facilitating Bow_SectionAngle, Bow_WaterlineAngle and Bow_FrontWidth

Geometry DefinitionBow

• a lofted surface connects the base curves

• side surfaces are simply extruded

Geometry DefinitionFlowpart

• flowpart and tunnel is created as one rotational brep

• the rotational brep is substractedfrom the hull brep

Geometry DefinitionTunnel Hull Transition

• Tunnel hull transition is created a linear edge fillet (huge benefit of breps!)

Geometry DefinitionSupport Geometry

• support curves are created based on brep edges

• they adapt to geometry changes

Geometry DefinitionSupport Geometry

• support curves are created based on brep edges

• they adapt to geometry changes

Grid GenerationHull Control Volume (Structured Hexahedron Approach)

Geometry DefinitionMesh Parameters

Grid GenerationFlowpart Study

Grid GenerationControl Volume

Control VolumeBoundary Definition

stat. pressure

slip wall

Rotor:noslip wall(rotational velocity)

stat. pressure

Post ProcessingBow Study

Standard Report Resistance Calculation

Automatic Latex Report CreationSupported by CAESES

• standard tool in project work

• often tank test results are not available for power predictions of our propellers

• or changes / enhancement on the hull have to be evaluated

• standardized hydrostatics, mesh generation, CFD setup, post processing and reporting

Main Views

Finished ReportExample

Conclusion

1. great tool – many possibilities (design studies, optimization and even different tasks)

2. excellent support – fast response on questions and also implementation of new features

3. main work horse – all our standard calculation are run through CAESES

The application of CAESES from a perspective of a

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