A 6-kip force is applied to the machine element AB as shown. Knowing that the uniform thickness of the element is 0.8 in., deter- mine the normal and shearing stresses at (a) point a, (b) point b, (c) point c. 8 in.- -8 in. 6 kips 35° A 8 in. B a d 1.5 in. 1.5 in. ob Oe- f

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A:

Q: Q1 The curved portion of the bar shown has an inner radius of 20 mm. Knowing that the allowable…

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Q: 4.17. Determine the components of stress from the results obtained in (a) v=rsin 0, ve = 2r cos 0…

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Q: Q2) The aluminum rod BC (G-26 GPa) is bonded to the brass rod AB (G-39 GPa). Knowing that Birass…

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Q: Two horizontal 8.51-kip forces are applied to pin B of the assembly shown. Knowing that a pin of…

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Q: T C. | I I Η Κ 10 kN 240 mm

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Q: (d) the average bearing stress at C in member BC, (e) the average bearing stress at B in member BC.

A:

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Q: The compressed-air tank AB has a 250-mm outside diameter and an 8-mm wall thickness. It is fitted…

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Q: Q1: A 6-kips force is applied to the machine element AB as shown. Knowing that the uniform thickness…

A: given data  P = 6 kips cross section = 0.8 × 3 in^2 find combined normal stress at point a and f.

Stress transformation

The term stress indicates the measure of internal forces that develop due to an external force's application on an object. When a specific external force is applied to an object, internal stress generates in the material. The value of stress can obtain by taking the ratio of the externally applied force and cross-sectional area of the object. There are different types of stress depending on the type of external force.