High order accurate and low dissipation method for unsteady compressible viscous flow computation on helicopter rotor in forward flight

DOI10.1016/j.jcp.2013.10.033zbMath1349.76555OpenAlexW2085445206MaRDI QIDQ348608

Li Xu, Pei-fen Weng

Publication date: 5 December 2016

Published in: Journal of Computational Physics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.jcp.2013.10.033

zbMATH Keywords

Navier-Stokes equationsunsteady flowsfull implicit dual time stepping methodlow dissipationmoving overset gridsWENO-Z scheme

Mathematics Subject Classification ID

Finite difference methods applied to problems in fluid mechanics (76M20) General aerodynamics and subsonic flows (76G25) Finite difference methods for initial value and initial-boundary value problems involving PDEs (65M06) Compressible fluids and gas dynamics (76Nxx)

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Cites Work

• Accuracy of the weighted essentially non-oscillatory conservative finite difference schemes
• Application of the principle of minimizing the derivative to the construction of finite-difference schemes for computing discontinuous solutions of gas dynamics. (Reprint)
• High order weighted essentially non-oscillatory WENO-Z schemes for hyperbolic conservation laws
• Rotor wake capture improvement based on high-order spatially accurate schemes and chimera grids
• WENO schemes based on upwind and centred TVD fluxes
• High resolution schemes for hyperbolic conservation laws
• Approximate Riemann solvers, parameter vectors, and difference schemes
• Weighted essentially non-oscillatory schemes
• Mapped weighted essentially non-oscillatory schemes: Achieving optimal order near critical points
• Efficient implementation of weighted ENO schemes
• Towards the ultimate conservative difference scheme. V. A second-order sequel to Godunov's method
• An improved weighted essentially non-oscillatory scheme for hyperbolic conservation laws
• Alternating direction implicit methods for the Navier-Stokes equations
• Chimera simulations of multibladed rotors in high-speed forward flight with weak fluid-structure-coupling

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