On the Numerical Prediction of Rotor Wakes Using Linear and Non-Linear Methods
暂无分享,去创建一个
[1] Siegfried Wagner,et al. Euler procedure for calculation of the steady rotor flow with emphasis on wake evolution , 1990 .
[2] B. Leer,et al. Flux-vector splitting for the Euler equations , 1997 .
[4] S. Wagner,et al. Compressible Potential Flow Around a Helicopter Rotor , 1995 .
[5] Earll M. Murman,et al. Total pressure loss in vortical solutions of the conical Euler equations , 1985 .
[6] S. Wagner,et al. Calculation of Blade-Vortex Interaction of Rotary Wings in Incompressible Flow by an Unsteady Vortex-Lattice Method Including Free Wake Analysis , 1992 .
[7] A. Eberle. 3D-Euler calculations using characteristic flux extrapolation , 1985 .
[8] Compressible potential flow around a helicopter rotor in arbitrary motion , 1996 .
[9] F. X. Caradonna,et al. Experimental and Analytical Studies of a Model Helicopter Rotor in Hover , 1980 .
[10] Antony Jameson,et al. LU implicit schemes with multiple grids for the Euler equations , 1986 .
[11] J. Hess. Panel Methods in Computational Fluid Dynamics , 1990 .
[12] A. J. Landgrebe. Overview of helicopter wake and airloads technology , 1985 .
[13] P. Roe. Approximate Riemann Solvers, Parameter Vectors, and Difference Schemes , 1997 .
[14] M. Liou,et al. A New Flux Splitting Scheme , 1993 .