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Research Output 1996 2017

  • 52 Citations
  • 5 h-Index
  • 20 Conference contribution
  • 14 Article
2017
Fluxes
Turbulence models
Reynolds number
Flow simulation
Airfoils
2016

Numerical simulation of transitional flow past a wing using flux reconstruction method

Skarolek, V. & Miyaji, K. 2016 In : AIAA Journal. 54, 4, p. 1424-1437 14 p.

Research output: Contribution to journalArticle

Fluxes
Large eddy simulation
Reynolds number
Polynomials
Unsteady flow
2015
1 Citations

Detached-eddy simulations of synthetic jets for high-angles-of-attack airfoils

Ishibashi, Y. & Miyaji, K. 2015 Jan 1 In : Journal of Aircraft. 52, 1, p. 168-175 8 p.

Research output: Contribution to journalArticle

Airfoils
Angle of attack
Orifices
Flow control
Drag

Study on Two-dimensional Wing Flutter Analysis by a High-order Flux Reconstruction Method

Morinaka, I. & Miyaji, K. 2015 In : Unknown Journal. 99, p. 543-550 8 p.

Research output: Contribution to journalArticle

Flutter (aerodynamics)
Fluxes
Subsonic flow
Transonic flow
Turbulence models
2014
8 Citations

An efficient correction procedure via reconstruction for simulation of viscous flow on moving and deforming domains

Liang, C., Miyaji, K. & Zhang, B. 2014 Jan 1 In : Journal of Computational Physics. 256, p. 55-68 14 p.

Research output: Contribution to journalArticle

Viscous flow
Conservation
Vortex flow
Fluxes
Derivatives

Detached eddy simulations of a synthetic jet for a high-angle-of-attack airfoil -inuence of the jet angle-

Ishibashi, Y. & Miyaji, K. 2014 52nd Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics Inc.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Airfoils
Angle of attack
Orifices
Flow control
Drag
1 Citations

Transitional flow over a SD7003 wing using flux reconstruction scheme

Skarolek, V. & Miyaji, K. 2014 52nd Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics Inc.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Fluxes
Large eddy simulation
Angle of attack
Reynolds number
Computer simulation

Transitional flow over a SD7003 wing using flux reconstruction scheme

Skarolek, V. & Miyaji, K. 2014 Jan 1 52nd AIAA Aerospace Sciences Meeting - AIAA Science and Technology Forum and Exposition, SciTech 2014. American Institute of Aeronautics and Astronautics Inc.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Fluxes
Large eddy simulation
Angle of attack
Reynolds number
Computer simulation

Unsteady flow over a SD7003 airfoil at low Reynolds numbers using a high-order accurate flux reconstruction scheme

Skarolek, V. & Miyaji, K. 2014 Jan 1 29th Congress of the International Council of the Aeronautical Sciences, ICAS 2014. International Council of the Aeronautical Sciences

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Fluxes
Reynolds number
Large eddy simulation
Unsteady flow
Angle of attack
2013

An efficient Correction Procedure via Reconstruction for simulation of viscous flow on moving and deforming domain

Liang, C., Miyaji, K. & Zhang, B. 2013 Aug 19 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition 2013.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Viscous flow
Conservation
Fluxes
Derivatives

Preface

Obayashi, S., Tamura, Y., Miyaji, K. & Shima, E. 2013 Oct 1 In : Computers and Fluids. 85

Research output: Contribution to journalArticle

2 Citations

Vortical flow simulations by a high-order accurate unstructured hexahedral grid method

Miyaji, K. 2013 Oct 1 In : Computers and Fluids. 85, p. 78-84 7 p.

Research output: Contribution to journalArticle

Fluxes
Vortex flow
Polynomials
Flow simulation
Derivatives
2012
6 Citations

Computational study of effects of nondimensional parameters on synthetic jets

Okada, K., Oyama, A., Fujii, K. & Miyaji, K. 2012 Feb 7 In : Transactions of the Japan Society for Aeronautical and Space Sciences. 55, 1, p. 1-11 11 p.

Research output: Contribution to journalArticle

Vortex flow
Large eddy simulation
Strouhal number
Orifices
Reynolds number

Tail-wing flutter analyses of a balloon-based operation vehicle for microgravity experiments

Miyaji, K., Machida, K., Fujita, K. & Sawai, S. 2012 Nov 1 In : Transactions of the Japan Society for Aeronautical and Space Sciences. 55, 6, p. 333-340 8 p.

Research output: Contribution to journalArticle

Balloons
Planforms
Flutter (aerodynamics)
Flight paths
Microgravity
2011

On the compressible flow simulations with shocks by a flux reconstruction approach

Miyaji, K. 2011 Dec 1 20th AIAA Computational Fluid Dynamics Conference 2011.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Fluxes
Compressible flow
Flow simulation
Shock problems
Finite difference method
2010

Computational study of frequency and amplitude effects on separation flow control with the synthetic jet

Okada, K., Fujii, K. & Miyaji, K. 2010 Jan 1 ASME International Mechanical Engineering Congress and Exposition, Proceedings. PART A ed. American Society of Mechanical Engineers (ASME), Vol. 9, p. 289-298 10 p.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Vortex flow
Large eddy simulation
Flow control
Navier Stokes equations
Flow fields

Computational study of the synthetic jet on separated flow over a backward-facing step

Okada, K., Fujii, K., Miyaji, K., Oyama, A., Nonomura, T. & Asada, K. 2010 Dec 1 ASME International Mechanical Engineering Congress and Exposition, Proceedings (IMECE). PARTS A AND B ed. Vol. 7, p. 161-170 10 p.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Vortex flow
Large eddy simulation
Navier Stokes equations
Numerical analysis
Flow fields

Flutter analysis of balloon-based operation vehicle for precooled turbojet engine demonstration

Miyaji, K., Matsuwaki, J., Kojima, T., Fujita, K. & Sawai, S. 2010 Dec 13 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. 2010-0055

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Flutter (aerodynamics)
Balloons
Turbojet engines
Planforms
Vibration analysis
2009

Effect of grid resolutions and injectant species in computations of supersonic mixing

Miyaji, K. & Kitazume, Y. 2009 Collection of Technical Papers - AIAA Applied Aerodynamics Conference.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Gases
Hypersonic aerodynamics
Shock waves
Computational fluid dynamics
Vortex flow
2008

Aerodynamic design of Balloon-based operation vehicle for precooled turbojet engine demonstration

Fujita, K., Tsuboi, N., Sawai, S., Kobayashi, H., Miyaji, K. & Uchiyama, T. 2008 Dec 1 15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. 2008-2658

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Balloons
Demonstrations
Turbojet engines
Aerodynamics
Engines
2006
11 Citations

Precooled turbojet engine flight experiment using balloon-based operation vehicle

Fujita, K., Sawai, S., Kobayashi, H., Tsuboi, N., Taguchi, H., Kojima, T., Okai, K., Sato, T. & Miyaji, K. 2006 Jul 1 In : Acta Astronautica. 59, 1-5, p. 263-270 8 p.

Research output: Contribution to journalArticle

Experiments
Turbojet engines
Balloons
Microgravity
Aerodynamic loads
2005

Comparisons between data-base and high-resolution simulations for shock/shock interactions

Miyaji, K. 2005 Dec 1 35th AIAA Fluid Dynamics Conference and Exhibit.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Shock waves
Aerodynamic heating
Hypersonic aerodynamics
Space flight
Adaptive algorithms

Numerical analysis of reverse jet effect on the aerodynamic characteristics of ssto configuration with an aerospike nozzle in landing phase

Fujimoto, K., Tsukada, H., Miyaji, K. & Fujii, K. 2005 Dec 1 International Astronautical Federation - 56th International Astronautical Congress 2005. Vol. 8, p. 5259-5269 11 p.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Nozzles
Aerodynamics
Flow interactions
Flow separation
Rockets

Numerical analysis of the aerodynamic characteristics of SSTO configurations with an aerospike nozzle

Tsukada, H., Fujimoto, K., Nonomura, T., Miyaji, K. & Fujii, K. 2005 Dec 1 43rd AIAA Aerospace Sciences Meeting and Exhibit - Meeting Papers. p. 9863-9872 10 p.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Drag coefficient
Angle of attack
Mach number
Aerodynamics
Supersonic flow
2004
9 Citations

High-order compact difference scheme applied to double-delta wing vortical flows

Arasawa, T., Fujii, K. & Miyaji, K. 2004 Jul 1 In : Journal of Aircraft. 41, 4, p. 953-957 5 p.

Research output: Contribution to journalArticle

Vortex flow
Flow simulation
Pressure distribution
Aircraft
2 Citations

On accuracy of prediction of flutter boundaries on unstructured grids

Miyaji, K., Tsukada, H. & Tsurumaki, A. 2004 Nov 1 In : Transactions of the Japan Society for Aeronautical and Space Sciences. 47, 157, p. 195-201 7 p.

Research output: Contribution to journalArticle

Flutter (aerodynamics)
Parallel flow
Flow simulation
2003

Application of high-order compact difference scheme to Vortical flow computation over a delta and double-delta wings

Arasawa, T., Fujii, K. & Miyaji, K. 2003 Dec 1 16th AIAA Computational Fluid Dynamics Conference.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Flow simulation
Pressure distribution
Vortex flow
Experiments

High-lift devices for a delta wing installed around a trailing-edge

Miyaji, K. & Arasawa, T. 2003 Sep 1 In : Journal of Aircraft. 40, 5, p. 932-937 6 p.

Research output: Contribution to journalArticle

Blow molding
Vortex flow
Angle of attack
Aerodynamics
2002

WEB-CFD and beyond-CFD for non-CFD researchers

Fujii, K. & Miyaji, K. 2002 Dec 1 40th AIAA Aerospace Sciences Meeting and Exhibit.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Computational fluid dynamics
HTML
Fluid dynamics
Aerospace applications
Flow simulation
2001

Prediction of hypersonic shock/shock interaction heating using hybrid adaptive unstructured grids

Miyaji, K. 2001 Dec 1 10th AIAA/NAL-NASDA-ISAS International Space Planes and Hypersonic Systems and Technologies Conference.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Shock waves
Heating rate
Aerodynamic heating
Hypersonic aerodynamics
Heating

Studies on high-lift devices for a delta wing installed around a trailing-edge

Miyaji, K. & Arasawa, T. 2001 Dec 1 19th AIAA Applied Aerodynamics Conference.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Blow molding
Vortex flow
Angle of attack
Aerodynamics
1999

Numerical analysis of three-dimensional shock/shock interactions and the aerodynamic heating

Miyaji, K. & Fujii, K. 1999 37th Aerospace Sciences Meeting and Exhibit. American Institute of Aeronautics and Astronautics Inc, AIAA, AIAA 99-0144

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Shock waves
Aerodynamic heating
Flow interactions
Hypersonic aerodynamics
Navier Stokes equations
1996
12 Citations

Enhancement of the leading-edge separation vortices by trailing-edge lateral blowing

Miyaji, K., Fujii, K. & Karashima, K. 1996 Sep 1 In : AIAA Journal. 34, 9, p. 1943-1945 3 p.

Research output: Contribution to journalArticle

Blow molding
Vortex flow

Unsteady behavior of the shock wave passing over two and three dimensional obstacles

Miyaji, K. & Fujii, K. 1996 14th Applied Aerodynamics Conference. American Institute of Aeronautics and Astronautics Inc, AIAA, p. 552-562 11 p. AIAA-96-2445

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Shock waves
Cones
Flow structure
Vortex flow