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SANDWICH BUCKLING

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SANDWICH BUCKLING AIAA Paper-97-1142 AIAA 38th SDM Meeting, 1997 A good review of sandwich walls Some earlier work on sandwich Some sandwich failure modes More ... – PowerPoint PPT presentation

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Title: SANDWICH BUCKLING


1
SANDWICH BUCKLING
  • AIAA Paper-97-1142
  • AIAA 38th SDM Meeting, 1997

2
(No Transcript)
3
A good review of sandwich walls
4
Some earlier work on sandwich
5
Some sandwich failure modes
6
More sandwich failure modes
7
Effect of initial face sheet wrinkling
Lcritical buckling (wrinkling) halfwave length.
Typical initial wrinkling amplitude, w0, is given
by w0/L0.001 (Plantema). Amplification of
initial face sheet wrinkling during axial
compression contributes to core crushing, face
sheet pull-off, core shear failure, stress in
sheet.
Initial face sheet waviness
Amplification of face sheet waviness under loading
8
Local buckling of stiffened panel
PANDA2 single module model, showing segments and
discretiza- tion for a T-stiffened panel.
Typical local buckling mode. See next slide for
web-skin interaction
9
Very local deformations of face sheet from
amplification of a possible local buckling
imperfection shape during loading
10
Face sheet wrinkling formulas from Vinson and
from Hoff
11
Face sheet wrinkling from Bushnell
Eigen-value
12
Amplification of initial face sheet waviness
during loading produces stress at core-facesheet
interface
13
Wrinkling halfwavelength and core cell size
constraint. Eq.(13)
14
What effects cause core crushing?
15
Typical core crushing allowable from a Hexcel
document
PSI
16
L and W directions in honeycomb sandwich core
The core shear stiffnesses and allowables differ
in the L and W directions.
17
Margins generated in PANDA2 from sandwich behavior
The next slide shows these two sets of margins
Face sheet 1
Face sheet 2
The 2nd slide shows this set.
Core
18
Detail showing face sheet margins
19
Detail showing core margins
20
Typical margins generated by PANDA2 for a
sandwich panel
21
Unstiffened sandwich plate, showing decision
variables, overall dimensions, and loading
This case is called VINSON in honor of
Professor Jack Vinson, the famous sandwich man!
22
Optimization by PANDA2 of the unstiffened panel
under various conditions
Eq(13) is the cell size constraint w0 is the
initial face sheet waviness amplitude L is the
wrinkling wavelength wimp is the amplitude of
the initial general buckling modal imperfection.
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