Engineering, 13.09.2019 23:10 preachersgirl5
Acarbon/epoxy (as/3501) unidirectional laminate with a fiber orientation q = 30° is exposed to the following stresses, sx = 40 ksi, sy = -20 ksi, txy = 20 ksi. determine the engineering strains in the fiber coordinate system. use the following typical properties for carbon/epoxy e1 = 18.4 msi, e2 = 1.6 msi, g12 = 0.95 msi, n12 = 0.28.
Answers: 2
Engineering, 04.07.2019 03:10
What precautions should you take to prevent injuries when dealing with heavy loads?
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Engineering, 04.07.2019 18:10
Items are similar to the free issue items, but their access is limited. (clo5) a)-bin stock items free issue b)-bin stock controlled issue c)-critical or insurance spares d)-rebuildable spares e)-consumables
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Engineering, 04.07.2019 18:10
Aturning operation is performed with following conditions: rake angle of 12°, a feed of 0.35 mm/rev, and a depth of cut of 1.1 mm. the work piece is aluminum alloy 6061 with t6 heat treatment (a16061-t6). the resultant chip thickness was measured to be 1.0 mm. estimate the cutting force, fc. use shear stress of 207 mpa and coefficient of friction on the tool face of 0.6.
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Engineering, 04.07.2019 18:20
Vibration monitoring this technique uses the noise or vibration created by mechanical equipment and in seme cases by plant systems to detemine their actual condtion. a)- true b)- false
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Acarbon/epoxy (as/3501) unidirectional laminate with a fiber orientation q = 30° is exposed to the f...
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