オープンソースとCFD Big Data/軽量化と信頼向上のための設計業務効率化   航空宇宙・重工業分野におけるCFDの応用と最適化/HPCクラウドコンピューティングと高速計算技術   FieldView・Pointwise・Phoenixワークショップ/TOSCAワークショップ
オープンソースとCFD Big Data 航空宇宙・重工業分野におけるCFDの応用と最適化
FieldView ワークショップ 10月9日(水)
Pointwise ワークショップ 10月9日(水)
Phoenix ワークショップ 10月9日(水)
軽量化と信頼向上のための設計業務効率化 HPCクラウドコンピューティングと高速計算技術
HPC Cloud Computing and High Speed Calculation Technology
8:30 – 9:00 Registration
9:00 – 9:40
Concept of CCNV, which supports implementation of HPC cloud computing in design process
Yasuhiko Fujikawa, President & CEO, VINAS Co., Ltd.
CCNV
9:40 – 10:20
Introduction and demonstration of CCNV multi cloud computing support system
Kenji Morimoto, Product Development, HPC Solution Department, VINAS Co., Ltd.
CCNV is a supporting system for managing the analysis jobs and data transfers that can use the multiple cloud computers and the internal server.
We demonstrate the function of CCNV which strongly support the usage of cloud computer, and also introduce new features, such as high speed file transfer.
CCNV
10:20 – 10:30 Break
10:30 – 11:10
Sponsor presentation
Evolving structure of visualization systems by remote GPU and virtualization technologies
Mr. Charlie Sugimoto, Director, Tesla Quadro Business Group, NVIDIA
Remote GPU and virtualization technologies enable various devices to be used remotely to perform visualization of 3D CAD and CAE, which used to be performed only by traditional work stations. This session provides introduction and demonstrations of these technologies.
11:10 – 11:50
Large-scale molecular simulations and drug design
Professor Shigenori Tanaka, Graduate School of System Informatics, Kobe University
ABINIT-MPBioStation
Ab initio electronic-state calculations of biomolecules based on the fragment molecular orbital (FMO) method have become easier to be performed by softwares such as ABINIT-MP/BioStation.
Possible analyses as well as anticipated future developments will be discussed.
11:50 – 13:20 Lunch / Demonstration *Short presentation
13:20 – 13:50
Sponsor presentation
Global HPC Innovation accelerated by AWS Cloud
Mr. Jamie Kinney, Principal Solution Architect, Worldwide Public Sector, Amazon Web Services
Now four years have passed since “Cloud First” policy was implemented in United States, Cloud Adoption in an HPC area is getting into a mainstream globally. This session introduce an overview of AWS Cloud service for an HPC segment and the latest status of HPC innovation by AWS Cloud through actual AWS use cases in NASA, CERN, JAXA and others.
13:50 – 14:30
Sponsor presentation
The Questions-Answering System Watson and its Medical Applications
Mr. Koichi Takeda, IBM Japan, Ltd.
I will introduce the technical impact of IBM's question-answering system Watson in the Jeopardy! challenge and its healthcare applications such as medical diagnosis support.
14:30 – 15:00
Introduction of high-performance computing consulting service
Naoyuki Sogo, High Speed Computation Technology Group, HPC Solution Department, VINAS Co., Ltd.
We will introduce our HPC consulting service which is based on the development experience of the hi-speed and robust matrix solver SMS over the years
Super Matrix Solver
15:00 – 15:30
Numerical prediction technologies for thermal flow phenomena accompanying boiling
Mr. Yutaka Umemura , Ph.D. (Aerospace Project Research Associate), Department of Aeronautics and Astronautics, The University of Tokyo
Super Matrix SolverCIP-LSM
In order to realize a space transportation vehicle for missions beyond the moon, establishment of technologies to predict thermal flow of cryogenic propellant is sought after.
Analysis results of thermal flow phenomena involving a phase change using CIP-LSM will be presented, as well as use of fast matrix solvers.
15:30 – 15:50 Coffee Break/Demonstration *Short presentation
15:50 – 16:20
Peta-scale computing in the field of solid mechanics
Associate Professor Tomonori Yamada , Ph. D., Research into Artifacts, Center for Engineering (RACE), The University of Tokyo
ADVENTURE
The leading supercomputers are offering peta-scale computing capability in the world. In Japan, the K-computer, one of the most advanced supercomputers in the world developed by a national project, and FX10, a commercial version of it, are two leading symbols. This presentation illustrates simulation techniques which utilizes such peta-flops machines for evaluation of structural integrity of important structures.
16:20 – 16:50
Performance tuning of Lagrangian Particle Tracking Library (LPIlib) in Large-Scale Distributed parallel environments
Naoyuki Sogo, High Speed Computation Technology Group, HPC Solution Department, VINAS Co., Ltd.
We are working on performance tuning of Lagrangian Particle Tracking Library (LPTlib) which was developed by RIKEN-AICS We will show some key points to obtain higher performance in Large-Scale Distributed parallel environment.
FromtFlow/Violet Cartesian
16:50 – 17:30
Sponsor presentation
Turbulent combustion modeling capabilities and application examples of NuFD/FrontFlowRed
Mr. Takayuki Nishiie, Researcher, Numerical Flow Designing CO., LTD.
NuFD/FrontFlowRed
NuFD/FrontFlowRed (FFR) contains advanced turbulent combustion modeling capabilities with the cooperation of researchers from universities and research institutes and provides highly accurate unsteady analysis of turbulent combustion flow using Large-Eddy Simulation. Turbulent combustion models and application examples of NuFD/FFR to industrial combustors will be introduced.
17:30 – 17:45
(Broadcasting)Closing Speech
Yasuhiko Fujikawa, President & CEO, VINAS Co., Ltd.

Application / Platform which will be used in the presentations

-Please note the program may change without prior notice.
-Company and product names are trademarks or registered trademarks.

Application of CFD and Optimization in Aerospace and Heavy Industries
8:30 – 9:00 Registration
9:00 – 9:15
Analysis examples of CRUNCH CFD V3.0 for technical solution of complicated fluid problem
Takeru Fukuchi, Manager, Engineering Department 1, VINAS Co., Ltd.
The major functions of CRUNCH CFD and new functions of the latest version V3.0 are introduced with the application examples and verification results to industrials field such as aerospace. In particular the application examples of difficult analysis using other CFD solvers are shown.
CRUNCH CFDFildViewPointwise
9:15 – 9:55
Advances in CRUNCH CFD® for efficient computation of complex moving body and unsteady applications.
Mr. Ashvin Hosangadi , Ph.D., Principal Scientist , Combustion Research and Flow Technology(CRAFT Tech)
CRUNCH CFDPointwiseGridgen
An overview of advances in CRUNCH CFD® for efficient analyses of complex moving body applications such as whirling seals and impellers, and deep-sea screw pumps will be provided. New techniques for unsteady design optimization will also be discussed.
9:55 – 10:25
CFD analysis of rocket-ramjet combined cycle engine using CRUNCH CFD
Mr. Masatoshi Kodera, Ph.D., Researcher, Space Transportation Mission Directorate, Japan Aerospace Exploration Agency (JAXA)
CRUNCH CFDFildView
In JAXA, we are conducting a research of rocket-ram/scramjet combined cycle engine as an engine for future space transportation systems. In this presentation, combustion analysis of the engine using CRUNCH CFD will be presented.
10:25 – 10:55
Pilot study of using AMAZON AWS and CRUNCH CFD for rocket engine development
Mr. Kaname Kawatsu, Engineer, JEDI Center, Japan Aerospace Exploration Agency (JAXA)
CCNVCRUNCH CFDFildViewGridgen
In our development process, many different kinds of simulations are conducted, which makes the amount of required computational resource vary considerably. Therefore, we have been considering using AMAZON AWS as a way of handling the varying requirements. Our trial use of it and results will be presented in this session.
10:55 – 11:10
TURBOdesign Suite 5.3 with enhanced 3D transonic viscous inverse design code.
Yukihiro Yamamoto, Product Group, Engineering Department 1, VINAS Co., Ltd.
Some topics about the next version "TURBOdesign Suite 5.3" will be shown. Some enhancement of modules, including TURBOdesign2, 3D Transonic Viscous Inverse Design Code, and TURBOdesign Pre, the meridional design by 1D sizing method, and so on.
TURBOdesign
11:10 – 11:50
Design of high performance Transonic/supersonic axial compressor and turbine stages by TURBOdesign
Professor Mehrdad Zangeneh Managing Director, Advanced design Technology
TURBOdesign
The presentation starts with an introduction to TURBOdesign2 and outline of some of the recent new functionalities implemented in the code. This is then followed by its application to optimization of a transonic axial compressor rotor and transonic LP turbine stage for gas turbine applications.
11:50 – 13:00 Lunch / Demonstration *Short presentation
13:00 – 13:40
Automotive blower design with Inverse method applied on wheel and volute
Dr. Manuel Henner, Fan System & Airflow Simulation Manager, Valeo Thermal Systems
TURBOdesign
Inverse design techniques are well suited to drive the conception of blowers used in automotive applications. Geometries proposed by the code TD1 from ADT were obtained in a short timeframe, and additional numerical simulations have shown the improvement in performances and the perfect adaptation of the volute to the wheel.
13:40 – 13:55
The new functionality “Shape Matching” of Sculptor V3.4
Yukihiro Yamamoto, Product Group, Engineering Department 1, VINAS Co., Ltd.
In the next version of Sculptor, the new functionality “Shape Matching”, which matches a model shape for analysis to target shape using morphing technology and optimization of Sculptor, is planning to be added. And then, application of the functionality, such as reverse engineering, multi-disciplinary optimization etc., will be proposed in this presentation.
SCULPTOR
13:55 – 14:35
Introducing Shape Matching and other new features in SCULPTOR
Mr. Mark D. Landon, Ph.D. , CTO, Optimal Solutions Software, LLC
SCULPTOR
SCULPTOR has proven to be a powerful tool for automatic shape optimization with CFD, FEA, and other CAE tools. Now it can be used to easily perform Shape Matching to get more value out of CAE models. Much time and money is invested into creating the models used for analysis and manufacturing. Shape Matching in Sculptor provides the ability to quickly morph models into target shapes so they can be used in more than one discipline.
14:35 – 15:05
Design of optimized hull form using Pointwise, SCULPTOR and OpenFOAM
Mr. Takehiro Ikeda, Ship Hydrodynamics Department R&D Division, AKISHIMA LABORATORIES (MITSUI ZOSEN) INC.
PointwiseSCULPTOROpenFOAM
As the regulation on CO2 emission from shipping has been strengthened recently, we are engaged in development of hull forms having higher energy saving performances. As an example of optimization of a hull form, one of our studies conducted by linking Pointwise, SCULPTOR and OpenFOAM together, will be illustrated in this presentation.
15:05 – 15:25 Coffee Break/Demonstration *Short presentation
15:25 – 15:40
Overview of ModelCenter 10.2 multipurpose optimized design process integration system
Nobuyuki Suzuki, Phoenix Group, Engineering Department 1, VINAS Co., Ltd.
Overview of the ModelCenter provided by the Phoenix, develop the automation and optimization system using workflow model. In addition, WEB application CenterLink expands use of workflow template model developed by ModelCenter to designers. And introduce AnalysisLibrary to manage the Simulation data.
Phoenix
15:40 – 16:20
A Model Based Engineering (MBE) Framework for Simulation Automation, Integration, Optimization and Data Management
Mr. Scott Woyak, Ph.D., President & CEO, Phoenix Integration
Phoenix
To reduce design cycles and costs while improving product performance and quality, simulation must be effectively applied early and across the entire product lifecycle. Model Based Engineering (MBE) attempts to achieve this goal by providing a common framework for managing engineering simulations and data.
16:20 – 17:00
Using MBSE to Evaluate Fractionated Space Systems
Mr. Steven Cornford, Ph.D., Senior Engineer, Strategic Systems Analysis Office, NASA Jet Propulsion Laboratory
Phoenix
A tool for evaluating the business case for fractionated space systems has been developed under the DARPA System F6 Program. It allows users to evaluate the costs and benefits of various system architectures and designs against a variety of uncertainty cases, or futures.
17:00 – 17:30
Current initiatives and future plan of Integration of Rockets flight simulation tool in JAXA.
Mr. Toshiaki Daibo, Engineer, Space Transportation Mission Directorate, Japan Aerospace Exploration Agency (JAXA)
Phoenix
In order to improve rocket flight simulation analysis for shortening analysis duration, develop integrating system to use more than 10 types of analysis tools by Phoenix Suite products. This presentation introduces JAXA initiatives and future plan for more improvement of the system.
17:30 – 17:45
Closing Speech
Yasuhiko Fujikawa, President & CEO, VINAS Co., Ltd.

Application / Platform which will be used in the presentations

-Please note the program may change without prior notice.
-Company and product names are trademarks or registered trademarks.

Hands-on experience and support corner
DAY 1
10:30 – 17:00

DAY 2
10:30 – 17:00
サポートコーナーイメージ写真
Available software for hands-on experience are:
FieldView、Pointwise、Gridgen、CCNV、Phoenix、TOSCA、SCULPTOR、TURBOdesign、CRUNCH CFD、OOFELIE Multiphysics、TransMagic、ICE Reporter、TurboReporter、T-REX Master、BladeMaster
Try first-hand our CFD/CAE software products with their sample models loaded. Rather than just watching demonstrations, you can have hands-on experiences here. Our staff engineers will be with you to help and to answer your questions regarding use of our software products.

* Feel free to stop by at any time for demos and hands-on experiences.