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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