GRAPE
v. 107
Overview
The GRAPE code (GRids about Airfoils using Poisson's Equation) is an elliptic
grid generator originally intended for isolated airfoils. The code was
written by Reece Sorenson at NASA Ames Research Center, and was modified
by Rod Chima at NASA Glenn to allow generation of periodic Ctype grids
for turbomachinery blades. Turbomachinery grids generated with GRAPE can be used directly with the RVCQ3D CFD code.
Applications
 Axial compressors and turbines
 Centrifugal impellers and radial diffusers (no splitters)
 Pumps
 Linear cascades
 Isolated airfoils
 Supports all options in Sorenson's original code
Grid Types
The geometry input to GRAPE is completely general. If you can generate
coordinates for your geometry, GRAPE can probably put put a grid around
it.
 Cgrids around blades
 C and Ogrids around airfoils
Features
 Arbitrary specification of inner and outer boundary points
 Several options for reclustering boundary points
 Interior points are generated as a solution of a Poisson equation.
 Forcing terms in the Poisson equation maintain grid spacing and angles
at the boundaries.
 Version 107 uses new monotone splines for accurate geometry definition.
Input and output
 Namelist input
 Airfoils are input in a Cartesian (x,y) coordinate system.
 Turbomachinery blades are input in a cylindrical (m,rbar*theta) system,
where m is the arc length along the surface and rbar is a mean radius.
 Grid files are written as binary data in standard PLOT3D format
 Grid files can be read directly by RVCQ3D.
 Minimal printed output
Computer and graphics requirements
GRAPE requires a Fortran 90 compiler and CFD visualization software for
use. Click the button below for more information.
Test cases included with GRAPE 107
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Cgrid, NASA rotor 37,
70 percent span 
Cgrid, NASA 6:1
centrifugal impeller 
Cgrid, Goldman annular
turbine vane 
Ogrid, Garabedian and Korn airfoil 
