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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