Vector algorithm for large-memory cyber 205 simulations of navier-stokes flows over delta wings

Computer Physics Reports - Tập 11 - Trang 137-164 - 1989
Arthur Rizzi

Tài liệu tham khảo

Carcaillet, 1986, Leading edge vortex flow over a 75 degree swept delta wing: experimental and computational results Newsome, 1987, Vortical flow aerodynamics — physical aspects and numerical simulation, AIAA Paper 87-0205 MacCormack, 1969, The effect of viscosity in hyper-velocity impact cratering, AIAA Paper 6-354 Beam, 1978, AIAA J., 16, 393, 10.2514/3.60901 Thomas, 1985, Upwind relaxation algorithms for the Navier-Stokes equations, AIAA Paper 85-1501 CP Rizzetta, 1986, AIAA J., 24, 237, 10.2514/3.9251 Fujii, 1984, Numerical simulation of the viscous flow over three-dimensional complicated geometries, AIAA paper 84-1550 Thomas, 1987, Navier-Stokes Computations of Vortical Flows Over Low Aspect ratio Wings, AIAA Paper 87-0207 Fujii, 1987, Numerical simulation of vortical flows over a strake-delta wing, AIAA Paper 87-1229 Jameson, 1981, Numerical solutions of the Euler equations by finite volume methods using Runge-Kutta time-stepping schemes, AIAA Paper 81-1259 Rizzi, 1982, AIAA J., 20, 1321, 10.2514/3.7981 Haase, 1984, Development of a Navier-Stokes method based on a finite volume technique for the unsteady Euler equations Agarwal, 1984, Computation of transonic viscous airfoil inlet, and wing flowfields, AIAA paper 84-1551 Swanson, 1984, A multistage time-stepping scheme for the Navier-Stokes equations, AIAA Paper 85-0035 Martinelli, 1986, A multigrid method for the Navier-Stokes equations, AIAA Paper 86-0208 Reister, 1986, Viscous pressure wave boundary layer interaction Vatsa, 1987, J. Aircraft, 24, 377, 10.2514/3.45456 Schwamborn, 1988, Simulation of the DFVLR-F5 wing experiment using a block-structured explicit Navier-Stokes method Peyret, 1983 Rizzi, 1984, J. Fluid Mechan, 148, 45, 10.1017/S002211208400224X Kordulla, 1983, AIAA J., 21, 917, 10.2514/3.8174 Müller, 1986, Runge-Kutta finite-volume simulation of laminar transonic flow over a NACA0012 airfoil using the Navier-Stokes equations, FFA TN 1986-60 Norton, 1984, Implicit finite difference schemes with non-simply connected grids — a novel approach, AIAA Paper 84-0003 Eriksson, 1985, J. Comp. Phys., 57, 90, 10.1016/0021-9991(85)90054-3 Gary, 1964, Math. Comp., 18, 1, 10.1090/S0025-5718-1964-0158553-3 MacCormack, 1975, A numerical method for solving the Navier-Stokes equations with application to shock-boundary layer interactions, AIAA Paper 75-1 Abarbanel, 1981, J. Comp. Phys., 41, 1, 10.1016/0021-9991(81)90077-2 Nordström, 1985, Stability criteria for a second order accurate, time-split finite volume scheme to solve the Navier-Stokes equation, FFA TN 1985-08 Müller, 1985, Navier-Stokes solution for hypersonic flow over an indented nosetip, AIAA Paper 85-1504 Eriksson, 1982, AIAA J., 20, 1313, 10.2514/3.7980 Lamar, 1987, Review of vortex flow flight projects on the F-1068, AIAA Paper No. 87-2346 CP Bannink, 1986, Experiments on the transonic flow over a delta wing at high angles of attack, 37 Bütefish, 1987, Three component LDA measurements on a 65° delta wing, DFVLR Bericht 222-87A34 Hartmann, 1986, S/European transonic vortex flow experiment — data lists of pressure measurements, DFVLR-IB 222-86 A 26