alem1s aonsalpn A rectangular plate is subjected to a plane stress state with principal stresses: σ,-67...
A rectangular plate in plane stress is subjected to normal stresses Ox =50 MPa, Oy = 25 MPa, and shear stress Txy = -12.5 MPa. The ratio of the magnitudes of the principal stresses (01/02) is approximately: (A) 3.5 (B) 2 (C) 2.8 (0)4
M15.3 Principal stresses in a rectangular tube scenes The rectangular tube is subjected to a transverse shear force of V = 230 kN and a bending moment of M = 530 kN-m, each acting in the directions shown. Determine the bending stress, the transverse shear stress magnitude, the principal stresses, and the maximum shear stress magnitude acting at location H. У Он (MPa) H 550 mm TH (MPa) 65 mm Op1 (MPa) X Op2 (MPa) 12 mm ITmax (MPa) wall...
Problem 73-2 An element in plane stress is subjected to stresses σ.-105 MPa, dry-75 MPa, and Try-25 MPa (see the figure for Prob. 7.2-2) Determine the principal stresses and show them on a sketch of a properly oriented element.
For the state of stress shown: a) Determine the in-plane principal stresses and the maximum in-plane shear stress. b) Show these stresses on a properly oriented element. c) Determine the maximum shear stress d) How do these (a, b, c) change if z = -20 MPa (20 MPa in compression)? With detialed explination please! Much appreciated 90 MPa 20 MPa 60 MPa
A large flat plate is subjected to constant-amplitude uniaxial cyclic tensile stresses of a maximum stress of 147 and a minimum stress of 32 MPa. If before testing the largest surface crack is 0.98 mm and the plain-strain fracture toughness of the plate is 33.4 MPa m1/2, estimate the fatigue life of the plate in cycles to failure. For the plate, m = 3.7 and A = 5.0 x 10-12 in MPa and meter units. Assume Y = 1.14
Question 15 (1 point) A material element is subjected to plane stress conditions. The stresses at the point of interest are as follows (units of MPa are assumed): 0x =-87 Oy =36 Txy =-77 Determine the normal strain in the z-direction, Ex, in microstrain (to one decimal place). So if the value is 18.4 E-06, just enter "18.4". You may assume Young's modulus is 72 GPa and Poisson's ratio is 0.3 for this material.
A cantilever beam, with a rectangular cross section, is subjected to loads P, Q and R, as illustrated in the figure below. Given, P 100 kN, Q 15 kN and R 10 kN, determine the principal stresses and the maximum in-plane shearing stress at point B. Also, determine the planes on which the principal stresses act, and the planes on which the maximum in-plane shear stress acts. The vertical dimension (depth) of the beam is 120 mm. 40 mmA 2...
t. For the given state of stress determine a) The principal plane and the principal stresses b) The masimum in-plane shear stress e) The average normal stress d) The erientation of the stress for each case e) Draw the Mohr circle → 35 MPa 60 N
An aluminium block is subjected to the following stresses in two of the three perpencicular directions: = 46 MPa σ,-24 MPa and an unkno vn stress in the third direction r the Young's modulus or the material is 10 GPa and Poisson's atio is 0 32 and ifit s known that the strain in the z-direction ε is equal lo zero use the generalised Hooke's law to determine the strain the x direction
The rectangular steel plate below measures 1 m x 0.5 m x 10 mm. Assume that the 1 m dimension is in the x-direction and the 0.5 m dimension is in the y-direction. The plate is made of a material with an elastic modulus of 200 GPa and Poisson's Ratio of 0.3. Suppose a uniform normal stress, Ox, of 125 MPa is applied in the x-direction a) Calculate the stress, ay, required to produce a transverse strain Ey 0 (in...