High order accurate and low dissipation method for unsteady compressible viscous flow computation on helicopter rotor in forward flight
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Li Xu | Peifen Weng | Li Xu | P. Weng
[1] Wai-Sun Don,et al. An improved weighted essentially non-oscillatory scheme for hyperbolic conservation laws , 2008, J. Comput. Phys..
[2] Lakshmi N. Sankar,et al. Hybrid Navier-Stokes/Free-Wake Method for Modeling Blade-Vortex Interactions , 2010 .
[3] Brian E. Wake,et al. Recent rotor wake simulation and modeling studies at United Technologies Corporation , 2000 .
[4] H. Lomax,et al. Thin-layer approximation and algebraic model for separated turbulent flows , 1978 .
[5] B. V. Leer,et al. Towards the Ultimate Conservative Difference Scheme , 1997 .
[6] A. Jameson,et al. Lower-upper Symmetric-Gauss-Seidel method for the Euler and Navier-Stokes equations , 1988 .
[7] A. Jameson. Time dependent calculations using multigrid, with applications to unsteady flows past airfoils and wings , 1991 .
[8] Robert L. Meakin,et al. On automating domain connectivity for overset grids , 1995 .
[9] Jasim Ahmad,et al. Helicopter rotor blade computation in unsteady flows using moving overset grids , 1996 .
[10] D. Whitfield,et al. Numerical simulation of a helicopter rotor in hover and forward flight , 1995 .
[11] Juan J. Alonso,et al. Time-accurate simulation of helicopter rotor flows including aeroelastic effects , 1997 .
[12] W. J. McCroskey. Vortex wakes of rotorcraft , 1995 .
[13] Robert E. Harris,et al. An Efficient Adaptive Cartesian Vorticity Transport Solver for Rotorcraft Flowfield Analysis , 2010 .
[14] A. T. Conlisk,et al. Modern helicopter rotor aerodynamics , 2001 .
[15] Robert Meakin. A new method for establishing intergrid communication among systems of overset grids , 1991 .
[16] Siegfried Wagner,et al. Tip Vortex Conservation on a Helicopter Main Rotor Using Vortex-Adapted Chimera Grids , 2007 .
[17] Chengjian He,et al. Modeling Rotor Wake Dynamics with Viscous Vortex Particle Method , 2008 .
[18] Berend G. van der Wall,et al. Chimera simulations of multibladed rotors in high-speed forward flight with weak fluid-structure-coupling , 2005 .
[19] Implicit multigrid algorithm for the Navier-Stokes equations , 1991 .
[20] F. X. Caradonna,et al. Experimental and Analytical Studies of a Model Helicopter Rotor in Hover , 1980 .
[21] S. Osher,et al. Weighted essentially non-oscillatory schemes , 1994 .
[22] Wai-Sun Don,et al. High order weighted essentially non-oscillatory WENO-Z schemes for hyperbolic conservation laws , 2011, J. Comput. Phys..
[23] J. M. Powers,et al. Mapped weighted essentially non-oscillatory schemes: Achieving optimal order near critical points , 2005 .
[24] Soohyung Park,et al. Euler and Navier-Stokes Simulations of Helicopter Rotor Blade in Forward Flight Using an Overlapped Grid Solver , 2009 .
[25] Wai-Sun Don,et al. Accuracy of the weighted essentially non-oscillatory conservative finite difference schemes , 2013, J. Comput. Phys..
[26] V. P. Kolgan,et al. Application of the principle of minimizing the derivative to the construction of finite-difference schemes for computing discontinuous solutions of gas dynamics , 2011, J. Comput. Phys..
[27] C. Angelopoulos. High resolution schemes for hyperbolic conservation laws , 1992 .
[28] Rohit Jain,et al. Capability Enhancements in Version 3 of the Helios High-Fidelity Rotorcraft Simulation Code , 2012 .
[29] Li Xu,et al. Rotor wake capture improvement based on high-order spatially accurate schemes and chimera grids , 2011 .
[30] Chi-Wang Shu,et al. Efficient Implementation of Weighted ENO Schemes , 1995 .
[31] Prabhu Ramachandran,et al. Approximate Riemann solvers for the Godunov SPH (GSPH) , 2014, J. Comput. Phys..
[32] Lakshmi N. Sankar,et al. Application of Higher Order Spatially Accurate Schemes to Rotors in Hover , 2006 .
[33] P. Roe. Approximate Riemann Solvers, Parameter Vectors, and Difference Schemes , 1997 .
[34] Lakshmi N. Sankar,et al. High-Order Essentially Nonoscillatory Schemes for Rotary-Wing Wake Computations , 2004 .
[35] Eleuterio F. Toro,et al. WENO schemes based on upwind and centred TVD fluxes , 2005 .