| A = |
|
in.2 |
| d = |
0.00 |
in. |
| tw = |
0.00 |
in. |
| bf = |
0.00 |
in. |
| tf = |
0.00 |
in. |
| k(des) = |
0.00 |
in. |
| k(det) = |
0.00 |
in. |
| gage = |
0.00 |
in. |
| wt/ft = |
0.00 |
plf |
| br/(2*tf) = |
0.00 |
|
| d/tw = |
0.00 |
|
| lx = |
0.00 |
in.4 |
| Sx = |
0.00 |
in.3 |
| rx = |
0.00 |
in. |
| y(bar) = |
0.00 |
in. |
| Zx = |
0.00 |
in.3 |
| yp = |
0.00 |
in. |
| ly = |
0.00 |
in.4 |
| Sy = |
0.00 |
in.3 |
| ry = |
0.00 |
in. |
| Zy = |
0.00 |
in.3 |
| Qs(50) = |
0.00 |
|
| J = |
0.00 |
in.^6 |
| Cw = |
0.00 |
|
| a = |
0.00 |
in. |
| ro(bar) = |
0.00 |
in. |
| H = |
0.00 |
|
| A = |
|
in.2 |
| d = |
0.00 |
in. |
| tw = |
0.00 |
in. |
| bf = |
0.00 |
in. |
| tf = |
0.00 |
in. |
| k(des) = |
0.00 |
in. |
| k(det) = |
0.00 |
in. |
| gage = |
0.00 |
in. |
| wt/ft = |
0.00 |
plf |
| br/(2*tf) = |
0.00 |
|
| d/tw = |
0.00 |
|
| lx = |
0.00 |
in.4 |
| Sx = |
0.00 |
in.3 |
| rx = |
0.00 |
in. |
| y(bar) = |
0.00 |
in. |
| Zx = |
0.00 |
in.3 |
| yp = |
0.00 |
in. |
| ly = |
0.00 |
in.4 |
| Sy = |
0.00 |
in.3 |
| ry = |
0.00 |
in. |
| Zy = |
0.00 |
in.3 |
| Qs(50) = |
0.00 |
|
| J = |
0.00 |
in.^6 |
| Cw = |
0.00 |
|
| a = |
0.00 |
in. |
| ro(bar) = |
0.00 |
in. |
| H = |
0.00 |
|
| A = |
|
in.2 |
| d = |
0.00 |
in. |
| tw = |
0.00 |
in. |
| bf = |
0.00 |
in. |
| tf = |
0.00 |
in. |
| k(des) = |
0.00 |
in. |
| k(det) = |
0.00 |
in. |
| gage = |
0.00 |
in. |
| wt/ft = |
0.00 |
plf |
| br/(2*tf) = |
0.00 |
|
| d/tw = |
0.00 |
|
| lx = |
0.00 |
in.4 |
| Sx = |
0.00 |
in.3 |
| rx = |
0.00 |
in. |
| y(bar) = |
0.00 |
in. |
| Zx = |
0.00 |
in.3 |
| yp = |
0.00 |
in. |
| ly = |
0.00 |
in.4 |
| Sy = |
0.00 |
in.3 |
| ry = |
0.00 |
in. |
| Zy = |
0.00 |
in.3 |
| Qs(50) = |
0.00 |
|
| J = |
0.00 |
in.^6 |
| Cw = |
0.00 |
|
| a = |
0.00 |
in. |
| ro(bar) = |
0.00 |
in. |
| H = |
0.00 |
|
| A = |
|
in.2 |
| d = |
0.00 |
in. |
| tw = |
0.00 |
in. |
| bf = |
0.00 |
in. |
| tf = |
0.00 |
in. |
| k = |
0.00 |
in. |
| T = |
0.00 |
in. |
| gage = |
0.00 |
in. |
| rts = |
0.00 |
in. |
| ho = |
0.00 |
in. |
| wt./ft. = |
0.00 |
plf. |
| eo = |
0.00 |
in. |
| lx = |
0.00 |
in.4 |
| Sx = |
0.00 |
in.3 |
| rx = |
0.00 |
in. |
| Zx = |
0.00 |
in.3 |
| ly = |
0.00 |
in.4 |
| Sy = |
0.00 |
in.3 |
| ry = |
0.00 |
in. |
| x(bar) = |
0.00 |
in. |
| Zy = |
0.00 |
in.3 |
| xp = |
0.00 |
in. |
| J = |
0.00 |
in.4 |
| Cw = |
0.00 |
in.^6 |
| a = |
0.00 |
in. |
| ro(bar) = |
0.00 |
in. |
| H = |
0.00 |
— |
| A = |
|
in.2 |
| d = |
0.00 |
in. |
| tw = |
0.00 |
in. |
| bf = |
0.00 |
in. |
| tf = |
0.00 |
in. |
| k = |
0.00 |
in. |
| T = |
0.00 |
in. |
| gage = |
0.00 |
in. |
| rts = |
0.00 |
in. |
| ho = |
0.00 |
in. |
| wt./ft. = |
0.00 |
plf. |
| eo = |
0.00 |
in. |
| lx = |
0.00 |
in.4 |
| Sx = |
0.00 |
in.3 |
| rx = |
0.00 |
in. |
| Zx = |
0.00 |
in.3 |
| ly = |
0.00 |
in.4 |
| Sy = |
0.00 |
in.3 |
| ry = |
0.00 |
in. |
| x(bar) = |
0.00 |
in. |
| Zy = |
0.00 |
in.3 |
| xp = |
0.00 |
in. |
| J = |
0.00 |
in.4 |
| Cw = |
0.00 |
in.^6 |
| a = |
0.00 |
in. |
| ro(bar) = |
0.00 |
in. |
| H = |
0.00 |
— |
| A = |
|
in.2 |
| d = |
|
in. |
| tw = |
|
in. |
| bf = |
|
in. |
| tf = |
|
in. |
| k(des) = |
|
in. |
| k(det) = |
|
in. |
| k1 = |
|
in. |
| T = |
|
in. |
| gage = |
|
in. |
| wt./ft. = |
|
plf. |
| bf/(2*tf) = |
|
— |
| h/tw |
|
— |
| lx = |
|
in.4 |
| Sx = |
|
in.3 |
| rx = |
|
in. |
| Zx = |
|
in.3 |
| ly = |
|
in.4 |
| Sy = |
|
in.3 |
| ry = |
|
in. |
| Zy = |
|
in.3 |
| rts = |
|
in. |
| ho = |
|
in. |
| J = |
|
in.4 |
| Cw = |
|
in.^6 |
| a = |
|
in. |
| Wno = |
|
in.2 |
| Sw= |
|
in.4 |
| Qf = |
|
in.3 |
| Qw = |
|
in.3 |
error: Copy is disabled
