A 3-D code for viscous cascade flow prediction was developed. The space discretization uses a cell-centered scheme with eigenvalue scaling to weigh the artificial dissipation terms. Computational efficiency of a four stage Runge-Kutta scheme is enhanced by using variable coefficients, implicit residual smoothing, and a full multigrid method. The Baldwin-Lomax eddy viscosity model is used for turbulence closure. A zonal, nonperiodic grid is used to minimize mesh distortion in and downstream of the throat region. Applications are presented for an annular vane with and without end wall contouring, and for a large scale linear cascade. The calculation is validated by comparing with experiments and by studying grid dependency
The overall objective of the research carried out over the last two years was the development of new...
The development of a design/analysis flow solver at NASA Lewis Research Center is discussed. The sol...
A vertex based finite volume method for the solution of the three dimensional Reynolds averaged Navi...
A three-dimensional code for rotating blade-row flow analysis was developed. The space discretizatio...
A 3-D Navier-Stokes code has been developed for analysis of turbomachinery blade rows and other inte...
A new kind of C-type grid is proposed, this grid is non-periodic on the wake and allows minimum skew...
A new kind of C-type grid is proposed for turbomachinery flow calculations. This grid is nonperiodic...
The three dimensional viscous flow through a planar turbine cascade is numerically simulated by dire...
A vertex-based finite volume method for solving the three-dimensional compressible Reynolds-averaged...
An assessment of several three-dimensional computer codes used at the NASA Lewis Research Center is ...
An algebraic turbulence model is proposed for use with three-dimensional Navier-Stokes analyses. It ...
A quasi- three-dimensional rotor viscous code is used to predict high subsonic flow through an annu...
This work outlines a procedure for simulating the flow field within multistage turbomachinery which ...
A method Is presented for solving turbulent flow problems on three-dimensional unstructured grids. S...
A parallel multi-block Navier-Stokes solver with the k-ω turbulence model is developed to simulate t...
The overall objective of the research carried out over the last two years was the development of new...
The development of a design/analysis flow solver at NASA Lewis Research Center is discussed. The sol...
A vertex based finite volume method for the solution of the three dimensional Reynolds averaged Navi...
A three-dimensional code for rotating blade-row flow analysis was developed. The space discretizatio...
A 3-D Navier-Stokes code has been developed for analysis of turbomachinery blade rows and other inte...
A new kind of C-type grid is proposed, this grid is non-periodic on the wake and allows minimum skew...
A new kind of C-type grid is proposed for turbomachinery flow calculations. This grid is nonperiodic...
The three dimensional viscous flow through a planar turbine cascade is numerically simulated by dire...
A vertex-based finite volume method for solving the three-dimensional compressible Reynolds-averaged...
An assessment of several three-dimensional computer codes used at the NASA Lewis Research Center is ...
An algebraic turbulence model is proposed for use with three-dimensional Navier-Stokes analyses. It ...
A quasi- three-dimensional rotor viscous code is used to predict high subsonic flow through an annu...
This work outlines a procedure for simulating the flow field within multistage turbomachinery which ...
A method Is presented for solving turbulent flow problems on three-dimensional unstructured grids. S...
A parallel multi-block Navier-Stokes solver with the k-ω turbulence model is developed to simulate t...
The overall objective of the research carried out over the last two years was the development of new...
The development of a design/analysis flow solver at NASA Lewis Research Center is discussed. The sol...
A vertex based finite volume method for the solution of the three dimensional Reynolds averaged Navi...