ICE Roadmap Japanese STAR Conference Richard Johns Introduction - - PowerPoint PPT Presentation

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ICE Roadmap Japanese STAR Conference Richard Johns Introduction - - PowerPoint PPT Presentation

ICE Roadmap Japanese STAR Conference Richard Johns Introduction Top-Level Roadmap STAR-CCM+ and Internal Combustion Engines Modeling Improvements and Research Support Sprays LES Chemistry Meshing Summary Top-Level


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SLIDE 1

ICE Roadmap Japanese STAR Conference

Richard Johns

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SLIDE 2

Introduction

  • Top-Level Roadmap
  • STAR-CCM+ and Internal Combustion Engines
  • Modeling Improvements and Research Support
  • Sprays
  • LES
  • Chemistry
  • Meshing
  • Summary
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SLIDE 3

Top-Level Roadmap for In-Cylinder CFD

STAR STAR-CD CD STAR STAR-CCM CCM+

ICE Model dels Knowled wledge Experience perience New w Meshing shing Tech chno nologies logies Will b ill be available ailable and d maintai intained ned for as lo long as is is requi quired red Will b ill bec ecome

  • me the

suc uccessor sor in in-cylinde ylinder code de Model del and d Best st Prac actice ice Refinemen inements

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SLIDE 4

Advantage of a Integrated STAR-CCM+ Solution

In In-Cylinder Cylinder Fuel el Inje ject ction ion and d Fuel el Sy System tem Superc ercharg harging ing Engine ine CHT T & St Struc uctural ural Analysis lysis Pis iston n undercrown dercrown cooling

  • ling

Cran ankcase/ kcase/oil

  • il splas

lash/ h/ bear arings/br ings/breather eather sys ystem em Intak ake/ e/Ex Exhaust haust System ems 1D 1D-3D coup upling ling Af Aftertreatm rtreatmen ent Optim imization ization

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SLIDE 5

The Development and Adoption of Mathematical Models

  • CD-adapco does not choose to be an “Inventor of Models””
  • We see our tasks as:
  • Model adopter
  • Implementation - Refinement, Generalization and

Industrialization

  • Validation
  • Development of Recommended Usage & Best

Practices

  • Dissemination
  • Benchmarking
  • Support
  • Further refinement in the light of experience
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SLIDE 6

Engineering-Level vs High Fidelity Models

Hig igh-Fidelit Fidelity y spr pray ay-break reakup up model

  • del

Engineering ineering-Le Level vel spr pray ay-break breakup up model del

  • Why do we support High-Fidelity Models?
  • We learn a lot about fundamental physics
  • If we can’t solve the problem in a HF model we certainly

won’t solve it in a EL model

  • Our objective is to deliver both HF and EL models
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SLIDE 7

University Research & “Research Clubs”

  • We actively support and fund a number of universities

around the world where there are strong ICE Research groups

  • We support and engage with many others – the following

slides are not a comprehensive list – just a brief summary

  • We also members of and/or participate in various research

“clubs”:

  • FVV, Germany
  • Support of industry-initiated university projects
  • DERC – Direct-Injection Engine Research Consortium
  • Univ of Wisconsin research club focused on

experimental and theoretical ICE fundamentals

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SLIDE 8

University Research

University of Modena, Italy Principal Investigator: Prof S Fontanesi Development and Application of LES and improved RANS models for flow, mixture distribution and knock University of Connecticut, US Principal Investigators: Professors Tianfeng Lu and Zhuyin Ren Chemistry mechanisms, solver speedup, reduced mechanisms, and mechanism reduction tools

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University Research

Penn State University, US Principal Investigator: Prof D Haworth Validation of in-cylinder Flow and Turbulence with experimental data, soot model development Doshisha University, Japan, Principal Investigator: Prof Senda Spray-Wall impingement modeling. fuel injection, spray heat & mass transfer, flash boiling

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University Research

University of Darmstadt, Germany Principal Investigator: Prof Janicka Validation of Flow and Turbulence with in-cylinder measurements Un Universi sity ty of Vien Vienna Principal Investigator: Prof Lauer Modeling of multicomponent fuels, wall effects, autoignition in gasoline engines

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SLIDE 11

University Research

Seoul National University (SNUAL) Principal Investigator: Prof Min Combustion and emissions modeling: flamelets, dual-fuel, level-set, knock ETH Zurich (Technical University) Principal Investigator: Dr Yuri Wright Combustion and emissions modeling: CMC, level-set, fuels, LES and DES in-cylinder flows

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SLIDE 12

Pamb mb = 1 120 0 kPa Pamb mb = 4 40 kPa Pin inj = 2 20 Mpa Tin inj = 100 0 C

Ref: Parrish ish & Zink, , GM R R&D, Ilass 2008 2008

  • Current injection systems and operating conditions can

lead to complex spray phenomena

Fuel Injection and Sprays

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SLIDE 13

Non-flashing vs flashing analysis

Non-flas lashing hing Fla lash shing ing Y is is th the mass ss frac action ion of n non-conde condensib nsible le gas as

Courtesy of Prof David Schmidt, University of Massachusetts

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SLIDE 14

Pintle nozzle – jet-string breakup

Pin intle le Noz

  • zzle

zle

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SLIDE 15

LES/VOF calculation of jet-string breakup

ATOMIC 5 deg sector

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Spray Modeling Strategy

  • Support of HF and EL projects to understand better and improve

physics modeling

  • Develop numerical and meshing technologies to support new

Engineering Level models that can be embodied into in-cylinder calculations

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In-Cylinder LES, mixture formation and Cyclic Variability

  • Ensemble or cycle-averaged CFD and measurements are an

approximation to reality

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SLIDE 18
  • Small-scale information lost in the averaging process

In-Cylinder LES, mixture formation and Cyclic Variability

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SLIDE 19

LES – Intake take Flow low Struct ructure ure

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SLIDE 20

Cy Cycled led-Averag veraged ed LES

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SLIDE 21

LES – multicycle flame development

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SLIDE 22

LES - 3D Results Insight:

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SLIDE 23

Prediction of COV

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In-Cylinder LES, mixture formation and Cyclic Variability

  • The Challenges:
  • Can we predict this successfully using High-Fidelity

modeling?

  • Can we derive an Engineering-Level model from the lessons

learned from a High-Fidelity model?

  • Are these modeling additions to our code or different ways of

processing existing solutions?

  • Are there other flow features, such as instabilities, that we

ignore at our peril?

  • Is there a first-mover advantage for an OEM in being an early-

adopter of high-end technology?

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SLIDE 25

Combustion Chemistry

  • Strengthened Team:
  • Graham Goldin
  • Karin Fröjd
  • DARS v2.10 release:
  • ECFM and PVM library generation incl dual-fuel
  • Extended Range Soot library
  • University Collaborations
  • Complex fuel chemistry (DME, biodiesel etc)
  • Soot modeling
  • Dual Fuel
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SLIDE 26

Meshing Technology

  • Meshing is important!
  • Automatic
  • Efficiency & consistency in a production environment
  • Optimization and automated shape-change
  • Accurate
  • The ability to capture boundary details and small-scale

phenomena and gradients, for example, sprays, spark ignition etc

  • Robust & Fast
  • Must be successful 99% of the time and add minimal
  • verhead
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Meshing Technology

  • We have/will have 3 meshing options:

1) Existing template/trimmed meshing

– es-ice today, being developed for STAR-CCM+

2) XMesher

based on multiple morphed meshes and solution mapping – STAR-CD and STAR-CCM+

3) Overset Mesh

– “Attachment” of individual meshes to components moving through a stationary background mesh

– STAR-CCM+ only

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SLIDE 28

Overset Mesh

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XMesher – Automated Meshing for ICE

  • Developed over the past ~3 years
  • Stage 1:
  • Fully automatic, full-cycle meshing
  • Tested successfully on ~30 different real engine cases
  • Close comparison of results with es-ice meshing
  • Will be released in 2015
  • Stage 2
  • Local mesh refinement linked to specific events
  • Embedded spray-adapted meshing
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SLIDE 30

XMesher Solution Strategy

Mesh generated at this time Mesh morphed in - time Mesh morphed in + time Solution mapped to next mesh

Constrained Polyhedra Core Cartesian Mesh Prism Layers Aligned valve-seat mesh

Solution Mapping Solution Continues Morphing

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SLIDE 31

XMesher

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Illustration of XMesher process

Initial Meshes are inserted automatically

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Meshes are morphed with piston and valve motions, tested and then additional meshes inserted as required

Illustration of XMesher process

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This cycle is repeated until meshes for the entire calculation have been generated.

Illustration of XMesher process

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Performance

  • Concurrent meshing/morphing is used. Typical

total time ~ ½ to 1 hour

2 4 8 # cores res 30 30 60 60 90 90 Tim ime (mins mins)

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Summary of Test Cases

Case Total Mesh Generation time (mins) Number

  • f Grids

Base Mesh (mm) Max No. of cells Min No.

  • f cells

#1 2v gasoline 22 19 1 666945 498419 #2 4v gasoline 33 20 2 691707 485946 #3 4v diesel 60 23 2 1994121 1397606 #4 4v gasoline 42 16 1 751447 538127 #5 4v gasoline 37 17 2 1473225 777593 #6 4v gasoline 30 18 1 895494 720668

+24 Furt rthe her r Ca Cases

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SLIDE 37

Cell Count through an engine cycle

1.5M 1.2M

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SLIDE 38

Vector Field

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XMesher – Stage 2

  • Objective is:
  • Physics-dependent local refinement
  • General spray-oriented meshing, including the possibility

if meshing inside the injector if required

  • In prototype stage now
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Physics-driven Locally-refined meshing

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SLIDE 41

Physics-driven Locally-refined meshing

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General Spray-Adapted Mesh

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General Spray-Adapted Mesh

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Summary

  • Major Commitment to developing a STAR-CCM+ ICE Solution
  • Continued Support for STAR-CD for as long as required by our

Customers – v4.24 in 2015

  • New automated accurate meshing coming in both STAR-CD

and STAR-CCM+

  • Focused physics research leading to an improved predictive

capability in key areas

  • Continued Support to deliver Best-in-Class Engineering

Solutions for ICE of all our Customers