A soid, crcular ber ABC consists of two segments, as shown in the figureOne segment has a diameter of d,- 56 mm and length of L- 1.40 m; the other segmert has a diameter of d - 48 mm and length of L-1.15 m.what is the alowable torque T in Nm) if the shear stress in not to xceed 30 MPa and the angle of tuat between the ends of the ber is not to enceed 1.207 (Aamume G-B0 GP.)Nm

Answered: Image /qna-images/answer/64b61d1b-325b-45e3-b292-1483b3e0de36.jpg

A soid, crcular ber ABC consists of two segments, as shown in the figure One segment has a diameter of d,- 56 mm and length of L,-1.40 m; the other segmert has a diameter of d, - 48 mm and length of L,-1.15 m. what in the alomable torque T in Nm) if the shear atress ia not to xceed 30 MP and the angle of twat between the ends of the ber is not to eceed 1.207 (Aamume G-DO GP.)

A soid, crcular ber ABC consists of two segments, as shown in the figure One segment has a diameter of d,- 56 mm and length of L,-1.40 m; the other segmert has a diameter of d, - 48 mm and length of L,-1.15 m. what in the alomable torque T in Nm) if the shear atress ia not to xceed 30 MP and the angle of twat between the ends of the ber is not to eceed 1.207 (Aamume G-DO GP.)

Structural Analysis

6th Edition

ISBN:9781337630931

Author:KASSIMALI, Aslam.

Publisher:KASSIMALI, Aslam.

Chapter2: Loads On Structures

Section: Chapter Questions

Problem 1P

See similar textbooks

Similar questions

1. THE MEMBERS OF THE STRUCTURE SHOWN BELOW WEIGH 2918 N/M, DETERMINE THE SMALLEST DIAMETER OF PIN THAT CAN BE USED AT A IF THE SHEARING STRESS IS LIMITED TO 34470 kfa. ASSUME SINGLE SHEAR. 1.20 m 1.80m 1,20 M 0.90 m
The bell crack mechanism shown in Figure is in equilibrium for an applied load of F1 = 15KN at A and F2 at C. The pin at B has a diameter of 12mm. The thickness of the bell crank is 8mm while the support bracket has a thickness of 6mm. The bell crank and the support bracket each have an ultimate bearing strength of 550 MPa. a %3D = 300 mm; b = 150 mm ; c = 100 mm; 0 = 65° %3D 30° (2) Bell crank B a Fi H-8 mm В Bracket 6 mm 6 mm Connection detail Determine the factor of safety in the support bracket with respect to the ultimate bearing strength.
A beam ABC with an overhang from B toC supports a uniform load of 200 lb/ft throughout itslength (see figure). The beam is a channel section withdimensions as shown in the figure. The moment of inertiaabout the z axis (the neutral axis) equals 8.13 in4.(a) Calculate the maximum tensile stress σt andmaximum compressive stress σc due to theuniform load.(b) Find the required span length a that results inthe ratio of larger to smaller compressive stressbeing equal to the ratio of larger to smaller tensilestress for the beam. Assume that the totallength L =a + b = 18 ft remains unchanged.
A steel cantilever beam 6 m in length is subjected to a concentrated load of 120 N acting at the free end of the bar. The cross section of the beam is shown below. deep. Determine the magnitude and location of the maximum tensile and compressive bending stresses in the beam. As usual, neglect the weight of the beam. 4mm 120 N 1mm 1mm 6mm 6m 1mm 4mm
5 - An aluminum circular shaft, fixed at both ends, is loaded by torques applied at points B and C, as shown in the figure. The bar material has a shear modulus G = 85 GPa. Plot the maximum shear stress and angle of twist along the length of the shaft. A D TB 0.5m Tc 0.9m с 0.4m 40mm ↑ TB-10KN-m Tc=15KN.m
Оиestion 3 Fig. 3a Part a: For the section shown, determine the: Maximum elastic Moment M 10 Fully plastic moment Mp NA Shape factor 2 If loaded about the horizontal axis o, = 250MN / m²; E = 200GN /m² 40 Part b: Determine the bending moment necessary to cause yielding to a depth of 10mm from the top and bottom surfaces. Fig. 3b If after applying this load it is subsequently removed. What will be the residual stresses NA which will result at A andB when the load is removed? Yielded region 40 09 09
الأول لمادة مقاومة المواد Question # 1: Determine the maximum shear stress acting at section a-a in the beam and the shearing stress at the junction of the flange and web plot the shearing stress along the beam. 200 mm 8000 N a 111 1.5 m 1.5 m 150 N/m 4 m G D 50 mm E 400 mm 75 mm 600 mm 75 mm
3. The beam is subjected to a shear of V-4 kN. Detemine the average shear stress developed in each nail if the nails are spaced 100 mm apart on each side of the beam. Each nail has a diameter of 4 mm. 100 mm 25 mm mm 75 mm mm 75 mi -75 nm 25 mm
2. Member AB shown in the figure supports a 5 N/mm uniformly distributed load and 4kN concentrated load as shown in the figure. Determine the position x of these loads so that the average tensile stress in the tie rod AC is equal to 90% of the compressive stress at the smooth support B. The rod has a diameter of 19 mm and the contact area at is 700mm². (Hint: quadratic formula) B A X 5 N/mm 4 kN 300mm B
9. A single horizontal force P of magnitude 900N is applied to end D of lever ABD shown in the figure below. Knowing that portion AB of the lever has a diameter 36mm, determine a) the normal and shearing stresses on an element located at point H and having sides parallel to the x and y axes, b) the principal planes and the principal stresses at point H. 300 mm 120 mm y B H A 540 mm 36 mm P D
Problem 6 For the structure shown in the figure, determine the normal and shear stresses at point A on the cross section of the pipe. at section a-a. mun 40 mm 300 mm 300 mm
The beam shown in Fig1.carries a concentrated load of W and a total distributed load of 8 W. Determine the maximum safe value W that will not exceed allowable stresses in tension of 60 MPa, in compression of 90 MPa, or in shear of 15 MPa. 1m W ᎦᎳ ? 15 2m 1m 20mm Fig.1 140mm 20mm 2 20mm 140mm