Chapter 40: Slides. Not done.
Fortran 77 implementation of high performance thin shell element used in aeroelastic studies of complete aircraft. Documentation at the start of each subroutine.
Mathematica Notebook version of above. Done by literal translation, statement by statement.
Plane beam with offset nodes covered in Sec 20.4 (added 4/19/09) of this IFEM Chapter. Beam stack material to be added.