JAXA Supercomputer System Annual Report April 2017-March 2018 Report Number: R17EB0101 Subject Category: Space Exploration Innovation PDF Responsible Representative: Kazuyoshi Kawasaki, Space Exploration Innovation Hub Center Contact Information: Takeshi Hoshino hoshino.takeshi@jaxa.jp Members: Takeshi Hoshino, Mitsuo Yamamoto, Inoue Hiroka Abstract Landing site selection and rover path planning on the Moon Reference URL N/A Reasons for using JSS2 Inspection of the result of parallelisation of simulation tools, estimation of thier execution times, and the execution of the simulation tools Achievements of the・・・<<read more>>
JAXA Supercomputer System Annual Report April 2017-March 2018 Report Number: R17ECMP04 Subject Category: Competitive Funding PDF Responsible Representative: Takuji Kurotaki, Aeronautical Technology Directorate, Numerical Simulation Research Unit Contact Information: Takuji Kurotraki kurotaki@chofu.jaxa.jp Members: Takuji Kurotaki Abstract Atomization of fuel of aeronautical engines is focused in because of fuel consumption and environmental issues. Information from CFD results is very helpful for solutions of them. The research of numerical simulation of compressible muti fluid flow is conducted to apply for these problems.・・・<<read more>>
JAXA Supercomputer System Annual Report April 2017-March 2018 Report Number: R17EA3211 Subject Category: Aeronautical Technology PDF Responsible Representative: Takeshi Ito, Aeronautical Technology Directorate, Next Generation Aeronautical Innovation Hub Center Contact Information: Shigeru Kuchi-Ishi shigeruk@chofu.jaxa.jp Members: Shigeru Kuchiishi, Minoru Yoshimoto, Shinsuke Nishimura, Yukinori Morita, Takuya Ogura Abstract An aerodynamic optimization tool by using the unstructured CFD code FaSTAR is developed. As a collaborative work with an airfcraft industory, an overset grid function of FaSTAR-Move, a CFD tool for moving/deforming body analysis,・・・<<read more>>
JAXA Supercomputer System Annual Report April 2017-March 2018 Report Number: R17EA0901 Subject Category: Aeronautical Technology PDF Responsible Representative: Shigeru Hamamoto, Aeronautical Technology Directorete, Aerodyamics Research Unit Contact Information: Yoshihisa Aoki aoki@chofu.jaxa.jp Members: Yoshihisa Aoki Abstract Improvement of aerodynamic characteristics of Quad Tilt Wing VTOL Plane in cruise. Reference URL N/A Reasons for using JSS2 It takes a lot of time to calculate using workstation. Achievements of the Year Wing aspect ratio sensitivity analysis of practical demonstration unmanned plane was conducted・・・<<read more>>
JAXA Supercomputer System Annual Report April 2017-March 2018 Report Number: R17EA2710 Subject Category: Aeronautical Technology PDF Responsible Representative: Toshio Nishizawa, aFJR Project Team, Aeronautical Technology Directorate Contact Information: Junichi Kazawa kazawa.junichi@jaxa.jp Members: Junichi Kazawa, Shunji Enomoto, Toshio Nishizawa, Susumu Kato, Kenshi Yamashita Abstract The purpose of aFJR project is to advance research on jet engine component technologies so that Japanese manufacturers can join more effectively in international joint-development projects on next-generation jet engines. To compensate for increasing fan diameter, we・・・<<read more>>
