Index
A-Basis values
adhesive
airframe
allowable
anti-symmetric laminate
aspect ratio
automated fiber/tow placement
balanced laminate
bathtub fittings
B-Basis values
beam
beam cross-section properties
bearing failure
bearing load
bearing of fasteners
bearing stress
bending stiffness of laminate
black aluminium
bolts (see fasteners)
bonding
boundary conditions
effect on beams
effect on beams on elastic foundation
effect on plates
buckling
beams
beams on elastic foundation
plates
building block approach
bulkhead
BVID
calculus of variations
cell size
clips
shear clips
tension clips
closed section beams
crippling
on plates
column buckling
complexity
core
double flex core
flex core
stabilization
corner
corrosion resistance
cost
assembly
cure cycle
labor
raw material
crimping (see shear crimping)
crippling
no-edge-free crippling
one-edge free crippling
under bending loads
cross-ply laminate
cross-section
properties
curvature
damage
deck
delamination
design
guidelines
process
requirements
values
diagonal tension
dimpling
doors
eccentricity (fittings)
effective skin
eigenvalue problem
generalized
standard
elastic foundation (see buckling)
energy
potential energy
complementary energy
environmental effects
equilibrium equations
equivalent properties
bending stiffness
membrane stiffness
Euler equations
external work
failure
first ply
material
failure index
failure mode
fasteners
filament winding
filler
finite element method
finite width correction factor
first ply failure
fit, form, ...
Get Design and Analysis of Composite Structures: With Applications to Aerospace Structures, 2nd Edition now with the O’Reilly learning platform.
O’Reilly members experience books, live events, courses curated by job role, and more from O’Reilly and nearly 200 top publishers.