Completed CFD Runs

The initial set of tests are to find the dependance of skin friction on wall jet amplitude at several detection planes. There are 129 grid points across the channel seperated non-uniformly and 64 grid points in both the streamwise and spanwise directions, with gridpoints being far closer together in the spanwise direction. The reynolds number is 180.

X= completed, O= in progress

y+\amp	-0.1	0.0	0.1	0.2	0.3	0.4	0.5	0.6	0.7	0.8	0.9	1.0	1.1	1.2	1.3
0		X
1
2
3
4
5
6
7
8
9
10	0			0			X			X		X
11	0			0			X			X		X
12	0			0			X			X		X
13	0			0			X			X		X
14	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-
15	0			0			X			X		X
16				0			0			X		X
17				0			0			X		X
18	-	-	-	-	-	-	-	-	-	-	-	-	-	-	-
19				0			0			X		X
20				X			X			X		X
21
22
23
24
25				X			X			X		X

 

 

Grid

Fortran Compiling

f77 -r8 -O4 chan*.f fourier.f

mv a.out y11-a05.out

nohup cfd.run &

compress test*/restrt24*.dat