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Photoelastic Stress Analysis [PDF]

open access: yes, 2009
Dubey, Venketesh N.
core  

Advanced manufacturing development of a composite empennage component for L-1011 aircraft. Phase 2: Design and analysis [PDF]

open access: yes
The composite fin design consists of two one-piece cocured covers, two one-piece cocured spars and eleven ribs. The lower ribs are truss ribs with graphite/epoxy caps and aluminum truss members.
Crocker, J. F.   +6 more
core   +1 more source

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