Add to ORKGThe three dimensional Navier-Stokes solution code using the LU-ADI factorization algorithm was employed to simulate the workshop test cases of transonic flow past a wing model in a wind tunnel and in free air. The effect of the tunnel walls is well demonstrated by the present simulations. An Amdahl 1200 supercomputer having 128 Mbytes main memory was used for these computations
A natural laminar flow (NLF) wind tunnel model has been designed and analyzed for a wind tunnel test...
The feasibility was determined of incorporating the Navier-Stokes computational code, CFL3D, into th...
The work performed during the past year on this cooperative agreement covered two major areas and tw...
The capabilities of an existing 3-D incompressible Navier-Stokes flow solver, INS3D, are extended an...
The transonic Navier-Stokes code was used to simulate flow fields about isolated wings for workshop ...
The two-dimensional (2-D) and three-dimensional Navier-Stokes equations are solved for flow over a N...
An explicit multistage Runge-Kutta type of time-stepping scheme is used for solving transonic flow p...
Critical to the advancement of computational aerodynamics capability is the ability to simulate flow...
The paper describes a numerical study of the high-speed leg of the NASA Langley 14 x 22-ft Low-Speed...
A computer analysis was developed for calculating steady (or unsteady) three-dimensional aircraft co...
A numerical simulation of the complete circuit of the NASA Langley 14 x 22-ft low-speed wind tunnel ...
Transonic flow fields about wing geometries are computed using an Euler/Navier-Stokes approach in wh...
Aeronautical applications of simulation technology at Ames Research Center are described. The larges...
For computational solution of the incompressible Navier-Stokes equations, the approximate factorizat...
Two codes which solve the 3-D Thin Layer Navier-Stokes (TLNS) equations are used to compute the stea...
A natural laminar flow (NLF) wind tunnel model has been designed and analyzed for a wind tunnel test...
The feasibility was determined of incorporating the Navier-Stokes computational code, CFL3D, into th...
The work performed during the past year on this cooperative agreement covered two major areas and tw...
The capabilities of an existing 3-D incompressible Navier-Stokes flow solver, INS3D, are extended an...
The transonic Navier-Stokes code was used to simulate flow fields about isolated wings for workshop ...
The two-dimensional (2-D) and three-dimensional Navier-Stokes equations are solved for flow over a N...
An explicit multistage Runge-Kutta type of time-stepping scheme is used for solving transonic flow p...
Critical to the advancement of computational aerodynamics capability is the ability to simulate flow...
The paper describes a numerical study of the high-speed leg of the NASA Langley 14 x 22-ft Low-Speed...
A computer analysis was developed for calculating steady (or unsteady) three-dimensional aircraft co...
A numerical simulation of the complete circuit of the NASA Langley 14 x 22-ft low-speed wind tunnel ...
Transonic flow fields about wing geometries are computed using an Euler/Navier-Stokes approach in wh...
Aeronautical applications of simulation technology at Ames Research Center are described. The larges...
For computational solution of the incompressible Navier-Stokes equations, the approximate factorizat...
Two codes which solve the 3-D Thin Layer Navier-Stokes (TLNS) equations are used to compute the stea...
A natural laminar flow (NLF) wind tunnel model has been designed and analyzed for a wind tunnel test...
The feasibility was determined of incorporating the Navier-Stokes computational code, CFL3D, into th...
The work performed during the past year on this cooperative agreement covered two major areas and tw...