A prismatic solid circular rod of diameter dis bent to introduce an offset s = das shown. The rod is further subjected to an axial load P. If the maximum longitudinal stress at a section A - B in the rod (with offset) is n times the longitudinal stress in straight rod, then the value of n would be Pt B +P A

A prismatic solid circular rod of diameter dis bent to introduce an offset s = das shown. The rod is further subjected to an axial load P. If the maximum longitudinal stress at a section A - B in the rod (with offset) is n times the longitudinal stress in straight rod, then the value of n would be Pt B +P A

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

3. For the given state of stress, determine the principal planes, the principal stresses, the max shear stress. You must use Mohr's Circle. 20 MPa 32 MPa 55 MPa
The bronze shaft is formed by attaching a hollow shaft to a solid shaft. The allowable shear stress of bronze is 100 MPa. Use G = 35 GPa for bronze. a. If the torque applied is 15 kN m, determine the maximum shearing stress developed in the bronze shaft b. Determine the maximum torque T that can be applied to the ends of the shaft without exceeding a shear stress of 100 MPa or an angle of twist of 3.5 in the 3.5-m length.
The compound shaft is attached to a rigid wall at each end. For the bronze segment AB, the diameter is 75 mm and G = 35 GPa. For the steel segment BC, the diameter is 50 mm and G = 83 GPa. Given that a = 2 m and b = 1.5 m, compute the largest torqueT that can be applied as shown in the figure if the maximum shear stress is limited to 60 MPa in the bronze and 80 MPa in the steel. 75 mm 50 mm A Bronze B Steel
Solve alll subparts b, c, d and e B) determine the principal plane (for σmax) in radians. C) Determine the shearing stress in a plane, which is 330 with the vertical (clockwise). D) determine the normal stress (in MPa) in a plane, which is 330 with the vertical (clockwise). E) determine the minimum values of θ (in radians) for which the normal stress is the equal to or less than 35.2 MPa.
The couple M=1.1 kN-m acts in a vertical plane and is applied to a beam oriented as shown. Determine the stress at point A 10 mm 40 mm The stress at point A is ( 10 mm 40 mm -10 mm 1,-1.894 x 10 mm 1,-0.614 x 10 mm +0.800 x 10 mm MPa.
Find the mayximum bending stress 75 N/m 60° N/m 2) 5m Ø Icm
4. Part AB of the bar has a solid circular cross section and part BC has a hollow circular cross section. The bar is fixed at both ends and a 150-in-kip axial torque is applied at B. Suppose that you want to decrease the weight of the bar by increasing the inside diameter of part B. The bar is made of material that will safely support a pure shear stress of 10 ksi. Based on this criterion, what is the largest safe value of the inside diameter? 4 in 2 in 150 in-kip A -14 in 7 in
Textbook: Statics and Strength of Materials Topic: Axial Shear and Bearing StressProvide step-by-step solutions.
The triangular plate is fixed at its base, and its apex A is given a horizontal displacement of 5 mm. Calculate the shear strain, Yxy, at A. Also, calculate the average normal strain & along the x' axis. 800 mm 45% 45° 800 mm 5 mm
The hollow circular beam is fixed to the wall (with a bracket) on the left and has an end-cap on the right. The cross-section is shown. (a) Determine state of stress at point A & draw the stress element (b) Determine state of stress at point B & draw the stress element A 100 k-in Tout 2 in n=1.75 in В. B 40 k-in C Tout 30 k X
All forces applied in the system are in the (x - y) plane. The material point B at the top of the beam is rotated at an angle of 15° counterclockwise. It is required that the shear stress is 12.5 MPa for this rotated material point B. At the bottom point A of the beam it is required that the maximum tensile stress is 110 MPa. Determine the load P and the length d that satisfies these constraints defined for points A and B. Given data: L = 4 b, t = b / 25, c = 2b, b = 600 mm, e = 5 , f = 12
What is the normal stress on the oblique plane due to the load P? 155 kip 7 in P = a = b = 4 in a = 37 degrees