JAXA Supercomputer System Annual Report
(April 2018-March 2019) Table of Contents
JAXA Supercomputer System Annual Report April 2018-March 2019
- Report pages could be accessed by clicking their titles. PDFs of individual reports are available in the report pages.
- Red “*” at the end of the report title indicates that it has video clip(s).
Aeronautical Technology
- Active Fluid Flow Control using DBD Plasma Actuators
- Aerodynamic Characteristics Improvement of Quad Tilt Wing VTOL Plane
- Aerothermodynamic data of Mars aerocapture by JONATHAN
- aFJR light weight sound absorption liner technology development *
- An attempt to develop a method for modeling holistic phenomena without a prerequisite knowledge
- Collaborative research : advancement of unsteady flow simulation tequnique
- Collarboration work on reseach and development for ecowing technology (future aircraft design)
- Comparison of Strain Distribution Between Results of Flight Test and Finite Element Analysis
- Computational Simulations for Aircraft Modification Design in the FQUROH Project
- Cooperative Research on High Lift Devices in the FQUROH Project
- Detection of origination for 3D unsteady aerodynamic phenomena (AEROSENS) *
- Development of 3D CFD core-software of automotive engine combustion chamber
- Development of a Many-block Method for Enabling an Extremely Fast Combustion LES
- Development of Aerodynamic Optimization Library: Harmonny
- Development of Aeroelastic Simulation Tool based on FaSTAR-Move
- Development of combustor simulation system based on physics understanding and modelling *
- Development of FaSTAR-Move
- Environment Conscious Aircraft Systems Research in Eco-wing Technology: CFD Code Modifications
- Environment Conscious Aircraft Systems Research in Eco-wing Technology:Aerodynamic System Design Technology
- Environment Conscious Aircraft Systems Research in Eco-wing Technology:Airframe-Engine Noise Reduction Technology
- High-Resolution, Efficient CFD Methods by Second Slope Limiter for Transonic Speeds
- Improvement of numerical analysis for internal flow with complicated configuration inside aero-engine
- Innovation for Design, Data-acquisition, Trouble-shoot and Certification in Aircraft Development: Acceleration and accuracy improvement of aerodynamic modeling
- Innovation for Design, Data-acquisition, Trouble-shoot and Certification in Aircraft Development: Basic Techniques for Real Flight Prediction
- Investigation of internal flow of aircraft combustor for En-Core Project.
- Next generation jet engine technology – development of high efficiency compressor design tecnology and aerodynamic performance prediciton –
- Noise suppression technology for aircraft jet engines
- Numerical Analyses on Hypersonic Experimental Aircraft
- Numerical analysis on atomization and spray combustion
- Research and development for system integration of silent supersonic airplane technologies
- Research of Multi-Physics Simulation Technology
- Research of unsteady flow simulation toward prediction of full-flight envelope
- Research on Airframe Noise Reduction Design in the FQUROH Project
- Research on High-Speed Rotorcraft Technology
- Research on the aircraft structures and advanced composite materials
- Research on the performance improvement of practical aero-engine fuel injector
- Study on multi-dimensional time series data analysis
- System Operation of the Digital/Analog-Hybrid Wind Tunnel (DAHWIN)
- Systematic improvement of build and comparison of aerodynamic models of aircraft
- Systematic improvement of build and comparison of aerodynamic models of aircraft (Indirect Reynolds number effect evaluation)
- Utilization of RCS Jet interaction for Reinforcing Attitude Contorol Ability
Common Business
Competitive Funding
- Fundamental Researches of Fluid and Combustion for the Hypersonic Flight
- Numerical Simulation of a Multiple Rotor UAV Inside Narrow Tunnels
- Optimization of rotor blade
- Post-K Priority Issue 8D: Research and development of core technology to innovate aircraft design and operation *
- Prediction of Aerodynamic Performance by Aerodynamic Interaction Between a Rotor and a Wing on Compound Helicopter
- SGS Stress Transport Equation-based SGS Modeling for Comprehensive LES Model
Cooperative Graduate School System
JSS2 Inter-University Research
- Computational Study on Aerodynamic Characteristics of Slender Body Configurations
- Construction of LES model for high Mach number multiphase flow based on DNS analysis
- Development and application of multiphase flow solver for moving object using Cartesian grid
- Discharge-flow coupling analysis of DBD plasma actuator
- Feedback Control of Flow Separation Using DBD Plasma Actuator
- High-fidelity numerical simulation of compressible turbulent flows
- Influence of Fineness Ratio on Aerodynamic Characteristics of Fight Vehicles
- Large Scale N-body simulation of Planet Formation : Effect of Fragmentation of Planetesimals.
- Magnetohydrodynamic modeling of space plasma processes
- Numerical investigation of combustible flows using the adaptive mesh refinement (AMR)
- Numerical Simulations of Fully Developed Turbulence
- Numerical Study of Ionization Structure and Shock Wave Propagation Toward Flight Performance Improvement of Beaming Propulsion
- Numerical study of the convective structure in Venus atmosphere
- Numerical Study on Combustible Flow in Supersonic Flight Engines and Rocket Engines
- Numerical Study on Rotor Performance of Mars Helicopter
- Physics and modeling of compressible thermal turbulent boundary layers
- Requirement analysis for LiteBIRD’s optical system
- Studies on nonlinear vortex dynamics in the later-stage of laminar-turbulent transition in compressible boundary layers
- Study of high-fidelity simulations for compressible turbulent flows and aeroacoustics around complicated geometries.
- Study on Data Staging Technique for Efficient Post-Process ing in Large-Scale CFD Computation
- The Effect of Protuberant Devices on Aerodynamic Characteristics of Slender Body Vehicle
- Three-dimensional MHD simulation of the solar wind acceleration
Research and Development
- Aeroacoustic simulation of launch vehicle at lift-off
- Combustion analysis technology
- Development of High-fidelity Re-entry Safety Analysis Methods
- Fundamental Studies of Methane RCS
- Fundamental Study on Fluid and Combustion for Hypersonic Flight (Evaluation of Influence of Turbulence Intensity)
- Liquid-Propellant Rocket System Simulation
- Long-term orbital environment prediction by orbital debris evolutionary model
- Numerical Simulation of Rocket Turbopumps
- Project support activity using numerical simulation
- Research for Future Transportation System (Research for Scramjet Engine Flow Path)
- Research on future space transportation technology
- Research on Radiation Protection Technology
- Study on Future Space Transportation System using Air-breathing Engines
- Upper Weather Prediction
Skills Acquisition System
- Basic research for system integration of silent supersonic airplane technologies
- CFD simulations of a wind turbine wake for rapid recovery of velocity deficits
- Environment Conscious Aircraft Systems Research in Eco-wing Technology
- Numerical study on low-speed buffet
- Research for Aircraft Aeroacoustic Noise Prediction Technologies
- Research of Lattice Boltzmann Method
- Research on combustor simulation
- Research on aircraft engine combustor simulation
- Research on engine intake simulation
- Research on three-dimensional buffet simulation
- Study on calculation method for chemical reactions in turbulent combustion
- Study on dynamic instability of a reentry capsule at transonic speed
- Technical Training on High-Speed Rotorcraft
Space and Astronautical Science
- Hayabusa2
- NLFFF calculation of the solar coronal magnetic field based on Hinode observations
- Numerical Plasma Simulation on Advanced Space Propulsion Systems
- Research and Development of Sample Return Capsule for future planetary exploration
- Research on Solid/Hybrid Rocket: Development of RANS Solver for of Swirling-Oxidizer-Flow-Type Hybrid Rocket using Flamelet Combustion Model
- Study of high speed fluid
Space Exploration Innovation
Space Technology
- Atmospheric Environmental Monitoring Simulation
- Data Processing, Archiving and Distributing of ALOS/PALSAR and ALOS-2/PALSAR-2
- Earth observation satellite data processing for GPM/DPR
- Greenhouse gases Observing SATellite (GOSAT) mission
- Greenhouse gases Observing SATellite-2 (GOSAT-2) Project
- Numerical analysis for Turbopumps
- Numerical Analysis of aerodynamic characteristics on H3 launch vehicle
- Numerical Simulations for H3 Rocket Development
- Precise Orbit Determination by using MADOCA on JSS2
- Research for data assimilation of satellite global rainfall map
- Research of Precipitation Measuring Mission
- Study on development of satellite-based ocean data assimilation system *
- Utilization of JSS2 for AMSR-E higher level data processing
Overview of JSS2 Usage
Colophon
JAXA Supercomputer System Annual Report April 2018-March 2019