Numerical simulation of multi-bladed rotors in lifting forward flight

[1]  Christian B Allen,et al.  Convergence of steady and unsteady formulations for inviscid hovering rotor solutions , 2003 .

[2]  Christian Allen,et al.  Time-stepping and grid effects on convergence of inviscid rotor flows , 2002 .

[3]  Christian B Allen,et al.  Multigrid convergence of inviscid fixed‐ and rotary‐wing flows , 2002 .

[4]  Christian B Allen,et al.  Multigrid acceleration of an upwind Euler method for hovering rotor flows , 2001, The Aeronautical Journal (1968).

[5]  Christian B Allen.  The effect of grid topology and density on inviscid hovering rotor solutions , 1999 .

[6]  Christian B Allen,et al.  First results of the EROS European unsteady Euler code on overlapping grids , 1998 .

[7]  Christian B Allen,et al.  GEROS: A European grid generator for rotorcraft simulation methods , 1998 .

[8]  Christian B Allen.  Grid adaptation for unsteady flow computations , 1997 .

[9]  C. B. Allen,et al.  The reduction of numerical entropy generated by unsteady Shockwaves , 1997, The Aeronautical Journal (1968).

[10]  Shigeru Obayashi,et al.  Freestream capturing for moving coordinates in three dimensions , 1992 .

[11]  J. F. Thompson,et al.  A general three-dimensional elliptic grid generation system on a composite block structure , 1987 .

[12]  L. Eriksson.  Generation of boundary-conforming grids around wing-body configurations using transfinite interpolation , 1982 .

[13]  W. J. Gordon,et al.  Construction of curvilinear co-ordinate systems and applications to mesh generation , 1973 .