upd ex

PetrKryslUCSD · Dec 15, 2024 · 0aa757c · 0aa757c
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diff --git a/examples/shells/statics/composite/Barbero/barbero_3_1_examples.jl b/examples/shells/statics/composite/Barbero/barbero_3_1_examples.jl
@@ -1,5 +1,5 @@
 """
-From Barbero's Finite Element Analysis using Abaqus ... book Example 3.1
+From Barbero's Finite Element Analysis using Abaqus ... book. Example 3.1
 
 Consider a simply supported square plate ax = ay = 2000 mm, laminated
 with AS4D/9310 (Table 3.1) in a [0/90]n configuration. The total laminate thickness is

diff --git a/examples/shells/statics/composite/nafems_r0031_3_examples.jl b/examples/shells/statics/composite/nafems_r0031_3_examples.jl
@@ -1,8 +1,10 @@
-
+"""
+From Barbero's Finite Element Analysis using Abaqus ... book. Example 3.7
+Here we actually solve the original benchmark:
+R0031(3): Three-layer sandwich shell under normal pressure loading
+"""
 module nafems_r0031_3_examples
-# From Barbero's Finite Element Analysis using Abaqus ... book Example 3.7
-# Here we actually solve original benchmark:
-# R0031(3): Three-layer sandwich shell under normal pressure loading
+
 using LinearAlgebra: norm, Transpose, mul!, I
 using FinEtools
 using FinEtools.AlgoBaseModule: solve_blocked!