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Transcription
MECHANICS OF MATERIALS PROBLEMS CURTISS-WRIGHT ENGINEERING
Course B-4 Seely: Arts. 29-41 CADETTES 16D-A-123
16D-1. Fig. 16D-l (a) shows a wood airplane rib. For convenience, assume
a chordwise load distribution as shown in (b), and draw complete
shear and moment diagrams for the rib.
16D-2. Using a load factor of 4, determine the maximum fiber unit stress
in the rib of problem 16D-l. Note that the resisting section for
moment at spar cut-outs consists of cap strips only.
16D-3. Determine, for the rib of problem 16D-l, the shearing unit stress
at the junction of cap strip and web on section A-A. Use a load
factor of 4.
[image]
Cap Strip
Cut-out for Spar
FIG. 16D-1
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