论文信息 - Application of an efficient 3-D multigrid Euler method (MGAERO) to complete aircraft configurations - 字舞流文

Application of an efficient 3-D multigrid Euler method (MGAERO) to complete aircraft configurations

B. Epstein | D. M. Tidd | D. J. Strash | A. Luntz | A. Nachshon | T. Rubin | A. Nachshon | A. Luntz | T. Rubin

[1] V. R. Stewart. Aerodynamic characteristics of a propulsive wing-canard concept at STOL speeds , 1985 .

[2] A. Jameson,et al. Numerical solution of the Euler equations by finite volume methods using Runge Kutta time stepping schemes , 1981 .

[3] A Jameson,et al. CALCULATION OF IN VISCID TRANSONIC FLOW OVER A COMPLETE AIRCRAFT , 1986 .

[4] A. Cenko,et al. TranAir applications to transonic flowfield predictions , 1991 .

[5] Stephen F. Wornom,et al. Relative efficiency and accuracy of two Navier-Stokes codes for simulating attached transonic flow over wings , 1990 .

[6] A. Jameson,et al. Improvements to the aircraft Euler method , 1987 .

[7] Willy Fritz. Numerical Grid Generation Around Complete Aircraft Configurations , 1986 .

[8] Russell M. Cummings,et al. Numerical simulation of high-incidence flow over the F-18 aircraft , 1990 .

[9] B. Epstein,et al. Multigrid Euler solver about arbitrary aircraft configurations with Cartesian grids and local refinement , 1989 .