JAXA Supercomputer System Annual Report
(April 2019-March 2020) Table of Contents
JAXA Supercomputer System Annual Report April 2019-March 2020
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- Red “*” at the end of the report title indicates that it has video clip(s).
Aeronautical Technology
- Active Flow Control using Plusma Actuators
- Advanced simulation of internal flow in rotating machinery
- Aerodynamic Simulations on Airframe Noise Reduction Technology (FQUROH+)
- Aerodynamic testing technology for reentering capsules
- An attempt to develop a method for modeling holistic phenomena without a prerequisite knowledge
- Cooperative Research on Airframe Noise Reduction Technology (FQUROH+) #1
- Cooperative Research on Airframe Noise Reduction Technology (FQUROH+) #2
- Cooperative Research: unsteady flow simulation with unstructured-grid CFD code
- Detection of origination for 3D unsteady aerodynamic phenomena
- Development of 3D CFD core-software of automotive engine combustion chamber
- Development of Aerodynamic Optimization Library: Harmonee
- Development of Aeroelastic Simulation Tool based on FaSTAR-Move
- Development of CFD technology to support design of aircraft combustor with real configuration.
- Development of combustor simulation system based on physics understanding and modelling
- Development of FaSTAR-Move
- Digital tuft; measurement system of surface phisycal quantity for aircraft
- 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
- FINE (Flight Investigation of skiN-friction reducing Eco-coating)
- Flight Demonstration of Gust Alleviation Technologies
- 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
- Investigation of Indirect Reynolds Number Effect
- Investigation of internal flow of aircraft combustor for En-Core Project.
- Laminar-turbulent transition simulation in aFJR High efficiency fan technology development *
- Next generation jet engine technology – development of high efficiency compressor design tecnology and aerodynamic performance prediciton –
- Noise suppression technology for aircraft jet engines *
- Nonlinear Aeroelastic Framework for Multi-fidelity Analysis
- 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 High-Speed Rotorcraft Technologies
- Research of Multi-Physics Simulation Technology
- Research of unsteady flow simulation toward prediction of full flight envelope
- Research on Airframe Noise Reduction Design (FQUROH+)
- Research on Techniques of Sound Absorbing Liner Analysis
- Research on the performance improvement of practical aero-engine fuel injector
- Simulation of impact damage in thin CFRP laminates
- Study of the Effect of Boundary Layer Ingestion (BLI) on Aircraft Propulsion
- 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
Common Business
- Development and maintenance of S&MA platform “Quality Engineering Tool”
- Development of fluid analysis system for turbomachinery using CFD software named UPACS
Competitive Funding
- Aerodynamic Investigation of a Multiple-Rotor Drone in Ground Effect
- Fundamental Researches of Fluid and Combustion for the Hypersonic Flight
- Investigation on the structure of rotating detonation wave
- JAXA-SUBARU Cooperative Research
- Optimization of rotor blade
- Post-K Priority Issue 8D: Research and development of core technology to innovate aircraft design and operation *
- SGS Stress Transport Equation-based SGS Modeling for Comprehensive LES Model
Cooperative Graduate School System
- Fundamental Research on Noise Generation Mechanisms from Airframe *
- Migration in gravitationally unstable protoplanetary discs
- Study on spacecraft dynamics
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
- Data staging technique for improving post-processing performance in large-scale CFD analysis
- Development and application of multiphase flow solver for moving object using Cartesian grid
- Direct numerical simulation for understanding on flow over vortex generators
- Discharge-flow coupling simulation of nanosecond-pulse-driven plasma actuator
- Feedback Control of Flow Separation Using DBD Plasma Actuator
- Fundamental study of propagation of one-dementional detonation waves
- High-fidelity numerical simulation of compressible turbulent flows
- Machine-learning based prediction of fluid dynamics
- Numerical investigation of combustible flows using the adaptive mesh refinement (AMR)
- Numerical modeling of space plasma processes
- Numerical Simulations of Fully Developed Turbulence
- Numerical Study of Breakdown and Shock Wave Structures for Improvement of Flight Perofmrnace in a Beamed-energy Vehicle
- 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
- Nunerical Study on Improvement of Airfoil Performance at Low Reynolds Number
- Physics and modeling of compressible thermal turbulent boundary layers
- Requirement analysis for LiteBIRD’s optical system
- Reynolds Number Effect on Aerodynamic Characteristics of Slender Bodies
- 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 Aerodynamic Characteristics and Flow Fields for Mars Exploration Airplane
- Supersonic and hypersonic aerodynamic characteristics of a projectile with shock wave interference
Research and Development
- Aeroacoustic simulation of launch vehicle at lift-off
- Combustion analysis technology
- Development of High-fidelity Re-entry Safety Analysis Methods
- Liquid-Propellant Propulsion System Simulation
- Long-term orbital environment prediction by orbital debris evolutionary model
- Numerical Simulation of Rocket Turbopumps
- Project support activity using numerical simulation
- Research on Radiation Protection Technology
- Reserch of Vasitation Lidar data using HPC
- 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 analysis of wind turbine wake
- Computational analysis of compound helicopter
- Environment Conscious Aircraft Systems Research in Eco-wing Technology:Aerodynamic System Design Technology
- Forward flight performance of multirotor
- High-spped rotorcrafts technology trainning
- Numerical Simulation of the Ram Combustor
- Numerical Study of Supresonic Intake
- Numerical study on low-speed buffet
- Research of Lattice Boltzmann Method
- Research on combustor simulation
- Study for Embedded Large Eddy Simulation
- Study on calculation method for chemical reactions in turbulent combustion
- Study on dynamic instability of a reentry capsule at transonic speed
Space and Astronautical Science
- NLFFF calculations of the solar coronal magnetic field based on Hinode observations
- Numerical Plasma Simulation on Advanced Space Propulsion Systems
- Plasma simulation for electric propulsion
- Research and Development of Sample Return Capsule for future planetary exploration
- Study of high speed fluid
Space Exploration
- Lunar landing site analyses
- System-level technical study for the future lunar polar exploration mission
Space Technology
- Acceleration of aerosol product retrieval algorithm for Earth observation satellite using Artificial Intelligence (AI)
- ALOS / PALSAR data processing for the entire observation period
- Atmospheric Environmental Monitoring Simulation
- 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 turbo pumps
- 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
- Retrieval of greenhouse gas concentrations from GOSAT-2 observations
- Study on development of satellite-based ocean data assimilation system
- Utilization of JSS2 for AMSR-E higher level data processing
- Utilization of JSS2 for GCOM-C satellite control and mission operations
Overview of JSS2 Usage
Colophon
JAXA Supercomputer System Annual Report April 2019-March 2020