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Air flow distribution control by a fluidic element

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JAXA Supercomputer System Annual Report April 2017-March 2018 Report Number: R17ETET18 Subject Category: Skills Acquisition System PDF Responsible Representative: Takashi Yamane, Aeronautical Technology Directorate, Propulsion Research Unit Contact Information: Seiji Yoshida yoshida.seiji@jaxa.jp Members: YOSHIDA Seiji(JAXA), Mitsumasa Makida(JAXA), Naoki Nakamura(ASIRI), Takeishi Ikumi(Waseda univ.) Abstract Lean combustion is promising to reduce nitrogen oxide emission from jet-engines. To solve combustion instability, that is a problem of lean combustion, a pilot burner for ensuring stable combustion and a main burner for performing lean, low-NOx・・・<<read more>>

Study of numerical simulation for three-dimensional buffet

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JAXA Supercomputer System Annual Report April 2017-March 2018 Report Number: R17ETET21 Subject Category: Skills Acquisition System PDF Responsible Representative: Takashi Aoyama, Aeronautical Technology Directorate, Numerical Simulation Research Unit Contact Information: Atsushi Hashimoto hashimoto.atsushi@jaxa.jp Members: Yoimi Kojima, Yoichi Saito Abstract Shock-wave/boundary layer interaction on the suction side of the wing at high Mach number and/or high angle of attack leads to large scale self-sustained motion of the shock wave. This phenomenon is called transonic buffet. The buffet leads to dangerous structural・・・<<read more>>

Research on combustor simulation

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JAXA Supercomputer System Annual Report April 2017-March 2018 Report Number: R17ETET23 Subject Category: Skills Acquisition System PDF Responsible Representative: Takashi Aoyama, Aeronautical Technology Directorate, Numerical Simulation Research Unit Contact Information: Rui Toyonaga toyonaga.l.0121@ruri.waseda.jp Members: Rui Toyonaga Abstract For the development of a jet engine combustor with high environmental compatibility, we develop the combustion calculation code that can capture the pressure propagation and chemical reaction with practical calculation cost. In addition, a verification calculation of this calculation code is conducted on・・・<<read more>>

Study on Aerodynamics of Space Plane

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JAXA Supercomputer System Annual Report April 2017-March 2018 Report Number: R17ETET24 Subject Category: Skills Acquisition System PDF Responsible Representative: Yusuke Maru, Department of Space Flight Systems, Institute of Space and Astronautical Science Contact Information: Yusuke Maru maru.yusuke@jaxa.jp Members: Mafuyu Imai, Tomoya Mukai Abstract Conducting aerodynamic design and evaluation of aerodynamic characteristics on space plane carrying amor breathing engines with CFD simulations. Reference URL N/A Reasons for using JSS2 Simulation environment is arranged well. And also, CFD software is substantial. Achievements・・・<<read more>>

Study of calculation method for chemical reactions in turbulent combustion

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JAXA Supercomputer System Annual Report April 2017-March 2018 Report Number: R17ETET25 Subject Category: Skills Acquisition System PDF Responsible Representative: Takashi Aoyama, Aeronautical Technology Directorate, Numerical Simulation Research Unit Contact Information: Yusuke Komatsu ksw.koma2@asagi.waseda.jp Members: Yusuke Komatsu Abstract For the purpose of realization of hypersonic transport, research and development aiming at demonstration of integrated control technology for aircraft / propulsion under hypersonic conditions is under way. It is difficult to acquire the data necessary for the performance evaluation of the ramjet・・・<<read more>>