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Study of high-fidelity numerical schemes for compressible turbulent flows

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Report Number: R16E0041 Responsible Representative: Soshi Kawai(Department of Aerospace Engineering, Tohoku University.) Contact Information: Soshi Kawai(kawai@cfd.mech.tohoku.ac.jp) Members: Hiroyuki Asada, Soshi Kawai Subject Category: Aviation(Body sound) Abstract Low-noise devices for reducing airframe noise of aircrafts have been studied and developed in many literature, but the details of interaction between each device are insufficiently investigated. This study develops discontinuous Galerkin (DG) based high-fidelity numerical schemes for compressible turbulent flows around aircrafts to enhance guidelines for designing next-generation low-noise aircrafts by clarifying the・・・<<read more>>

Development of a shock-capturing magnetohydrodynamic code, ‘OpenMHD’

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Report Number: R16E0040 Responsible Representative: Seiji Zenitani(National Astronomical Observatory of Japan, Division of Theoretical Astronomy) Contact Information: Seiji Zenitani(zenitani@rish.kyoto-u.ac.jp) Members: Tsugunobu Nagai, Seiji Zenitani Subject Category: Space(Space science,Space philosophy) Abstract We conduct scientifitc researches on basic processes in space plasma environments, by using numerical simulations. We also develop an open-source simulation code. Goal To conduct a scientific research on basic processes in space plasmas Objective To develop a magnetohydrodynamic (MHD) simulation code for space plasma research References and Links Please・・・<<read more>>

Numerical Study on Combustible Flow in supersonic Flight Engines and Rocket Engines

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Report Number: R16E0039 Responsible Representative: Nobuyuki Tsuboi(Department of Mechanical and Control Engineering, Kyushu Institute of Technology) Contact Information: Nobuyuki Tsuboi(tsuboi@mech.kyutech.ac.jp) Members: Satoshi Koduka, Maiko Iwai, Toshihiro Iwasa, Takahide Araki, Keisuke Fujimoto, Motaka Niibo, Moyuki Mutato, Seiichiro Eto, Keisuke Yoshida, Daiki Muto, Nobuyuki Tsuboi Subject Category: Space(Rocket engine,Space transportation) Abstract Reactive Fluid Dynamics Laboratory at Department of Mechanical and Control Engineering, Kyushu Institute of Technology has the following research keywords: (1)Numerical simulation(CFD) (2) Compressible andsupersonic/hypersonic flow (3)Combustion flow (4)Liquid rocket engine,・・・<<read more>>

Studies on real flight prediction

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Report Number: R16E0038 Responsible Representative: Takeshi Ito(Aeronautical Technology Directorate, Next Generation Aeronautical Innovation Hub Center) Contact Information: Kazuyuki Nakakita(nakakita@chofu.jaxa.jp) Members: Keiko Kawaguchi, Kazuyuki Nakakita, Kanako Yasue, Rie Tagai, Makoto Ueno, Seigo Koga, Mitsuhiro Murayama, Kentaro Tanaka, Tohru Hirai, Yasushi Ito, Keita Hatanaka, Kohji Suzuki, Takahiro Uchiyama, Hiroya Toriida Subject Category: Aviation(Aircraft) Abstract By applying the sophisticated data analysis techniques to unsteady CFD data, we develop a methodology to detecting the sign of unsteady aerodynamic phenomena including buffet. Goal Through a・・・<<read more>>

Conceptual Study of a High Speed Compound Helicopter for Innovative Air Transportation

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Report Number: R16E0037 Responsible Representative: Yoshikazu Makino(Next Generation Aeronautical Innovation Hub Center, Aeronautical Technology Directorate) Contact Information: Yasutada Tanabe(tan@chofu.jaxa.jp) Members: Masahiko Sugiura, Yasutada Tanabe, Hideaki Sugawara Subject Category: Aviation(Aircraft) Abstract In Fiscal Year 2016, aerodynamic data of a conceptual model that has been flight tested are obtained and used to validate the CFD tool rFlow3D developed for rotorcraft. The aerodynamic interactions between a main rotor and a wing are simulated. Reduction of the downloading on the wing by a trailing・・・<<read more>>