The tank of the air compressor is subjected to an internal pressure of 120 psi. The inner diameter of the tank is 22 in., and the wall thickness is 0.25 in. 01 = Part A Determine the hoop stress acting at point A. Express your answer in kilopounds per square inch to three significant figures. ANSWER: ksi 02 = Σ Tap image to zoom Part B Determine the longitudinal stress acting at point A. Express your answer in kilopounds per square inch to three significant figures. ANSWER: ksi

The tank of the air compressor is subjected to an internal pressure of 120 psi. The inner diameter of the tank is 22 in., and the wall thickness is 0.25 in. 01 = Part A Determine the hoop stress acting at point A. Express your answer in kilopounds per square inch to three significant figures. ANSWER: ksi 02 = Σ Tap image to zoom Part B Determine the longitudinal stress acting at point A. Express your answer in kilopounds per square inch to three significant figures. ANSWER: ksi

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

What is the shearing stress developed at the neutral axis of the beam with a circular cross section having a diameter of 17 mm and a shear force V = 29 kN. Assume that the shearing stress is uniformly distributed across the neutral axis. Answer must be in MPa.
Determine the normal stress in the steel plate. Gusset plate is 16 mm thick column pin diameter = 20 mm gusset plate steel plate 70 kN pin 60mm 8-mm plate thickness 183.45 MP 0148.53 MPa 58.33 MP3 22282 MP A 14583MP
CLO 1: A rigid beam rests on two bronze bars 700 mm long. Another aluminum bar is placed between them which is 699.93 mm long. If the weight of the beam is 375 KN, determine the stress in bronze bar (in MPa). Bronze Bronze Alum Alum Bronze A in mm2 850 1500 E in Gpa 70 83 144.21 102.49 341.33 54.56
4 m 450 mm [s0 mn [50 mn 18 350 mm 50 mm Figure la Figure Ib Before a diver jumps into the water, helshe stands at point C, causing a deflection of the board A-B-C in the figure. The board A-B8-C has a modulus of elasticity of E = 15 MPa with the sketched dimensions and cross-section (fig. 1b). Assume g=10 mis?. Provide all steps of your working and solutions handwriten; include diagrams and coordinate systems. a. Determine the reactions at each support A and B. Use the variable w for the weight of the diver, include a free-body diagram.
Situation H. A 100m tape weighing 3kg that is standard at 10°C and a 30N pull is used to measure a distance which was recorded to be 3300m. Condition during survey: Modulus of Elasticity Temperature Pull 200 GPa 15 °C 40N Coefficient of 11.6 x 10-/°C Thermal Expansion 16. Determine the error due to sag. 17. Determine the error due to change in temperature. 18. Determine the error due to change in pull. 19. Determine the correct distance between the two points.
A 52-kip force acts on a machine part at point A as shown below. The diagram shows the internal normal force, shear force and bending moment acting on a particular RECTANGULAR Cross section. -30in N 10in 26in F=52 kip The value of the bending moment M you would use to find the bending stress on a stress element located 2 inches up from the bottom of the rectangular cross section is closest to: 264 kip-in O a. 408 kip-in Ob. 1,464 kip-in O c. 1,608 kip-in
Refer to the photo provided. Please make sure your handwriting is readable. Internal pressure and axial tensile force are applied to an open cylindrical tank 605 mm in diameter and 3.02 mm thick, resulting in the final stresses illustrated in the Mohr's circle. If a = 40.10 MPa, b = 100.06 MPa, and c = 45.05 MPa. 1. Determine the kPa value of the internal pressure. 2. What is the axial force's magnitude in kN?
The beam is subjected to a bending moment of M = 17 kN. m. σA = B 200 mm OB = 30 mm 30 mm M 30 mm 30 mm 50 mm 150 mm 150 mm 50 mm Part A Determine the bending stress in the beam at point A. Express your answer to three significant figures and include the appropriate units. Enter negative value in the case of compression and positive in the case of tension. ANSWER: Q Tap image to zoom Part B Determine the bending stress in the beam at point B. Express your answer to three significant figures and include the appropriate units. Enter negative value in the case of compression and positive in the case of tension. ANSWER:
Determine the shear strain Yxy at corners D and the plastic distorts as shown by the dashed lines. 3 mm 300 mm D 4 mm -400 mm- 12 mm B |A 5 mm 8 mm 12 mm X
The box wrench is subjected to the 50 lb force. (Figure 1) Figure 2 in. a 12 in. 0.5 in. A B Section a-a 1 of 1 50 lb Part A If t, determine the principal stress at point B on the cross section of the wrench at section a-a. Express your answers using three significant figures separated by a comma. VG ΑΣΦ [41 01.02 Submit Part B * Incorrect; Try Again; 29 attempts remaining Previous Answers Request Answer Tmax in-plane = vec Determine the maximum in-plane shear stress at point B on the cross section of the wrench at section a-a. Express your answer to three significant figures and include the appropriate units. μA Provide Feedback Value Submit Previous Answers Request Answer [w] ? Units * Incorrect; Try Again; 28 attempts remaining ? ksi
The drill is jammed in the wall and is subjected to the torque and force shown in a 20 N-m O A 125 mm = B 400 mm -5 mm Section a-a Part A Determine the normal stress at point A on the cross section of drill bit at section a-a. 150 N Express your answer to three significant figures and include the appropriate units. Enter negative value in the case of compression and positive value in the case of tension. ANSWER: Tap image to zoom ANSWER: ((Txy)V) A = Part B Determine the transverse stress at point A on the cross section of drill bit at section a-a. Express your answer to three significant figures and include the appropriate units.
Problem 5 The load has a weight of 950 lb. -1.5 ft- 1 in. max = Section a - a Q Tap image to zoom Part A Determine the maximum normal stress developed on the cross section of the supporting member at section a-a. Express your answer in kilopounds per square inch to three significant figures. Enter negative value in the case of compression and positive value in the case of tension. ANSWER: ksi