45° B. C 450
Chapter2: Loads On Structures
Section: Chapter Questions
Problem 1P
Related questions
Question
During a test of an airplane wing, the strain
gage readings from a 45° rosette (see figure) are as
follows: gage A, 520 X10-6 ; gage B, 360 X10-6 ; and
gage C, 280 X10-6 .
Determine the principal strains and maximum
shear strains, and show them on sketches of properly
oriented elements.
Transcribed Image Text:45°
B.
C
450
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