Consider the beam with properties and loadings as described in the figure and parameter table. Use superposition to find the angles of deflection at A and C (in degrees). M parameter W M Alloy Beam Type 0A = -3.71 L 0c = 4.34 A ** value A992 Steel W310 x 67 X X 6 50 65 O -L- units m kN/m kN-m B W -L- C
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- Consider the cantilevered W14 x 30 beam shown in (Eigure 1). E-29(10) ksi, I-291 in Figure <10f1 Skip Part A Determine the expression for the elastic curve using the coordinate z for 05a59ft, where is in feet Express your answer in terms of z. Express your answer using three significant figures. AX+ IT vec Submit Previous Answers Request Answer X Incorrect; Try Again; 5 attempts remaining Part B Determine the maximum slope of the beam, measured counterclockwise from the positive z axis Express your answer using three significant figures VAX Ivec Previous Arawers Request Aca X Incorrect; Try Again; 5 attempts remaining Submit ft ? radConsider the beam with properties and loadings as described in the figure and parameter table. Use superposition to find the angles of deflection at A and C (in degrees). M neo 0A = A 0c= 7////////// CC 2022 Cathy Zupke parameter L W BY NC SA Alloy Beam Type value 6 50 65 A992 Steel W310 x 67 O B O units W m kN/m kN m . C1. In figure (1), shows a uniform beam subjected to a linear increasing distributed load. The equation for the resulting elastic curve is: w y = 120EIL (-x5+2L?x3 - L*x) Using the numerical methods to determine the point of max. deflection (that is, the value of x where "Y 0. Then substitute dx this value in the given equation to find the value of maximum deflection. Using the following parameter values in your computations: L = 600cm; E50000 k N/cm2;1=30000cm* and w =2.5k N/cm. (a) r Ly 0) =0, v- 0) (b) Figure (1)
- Part A Consider the beam shown in (Figure 1). Suppose that the distributed load w = 700 lb/ft Follow the sign convention. Figure Vc = Submit Part B 900 lb-ft Mc = -3 (1 μÀ Value Qubmait Determine the internal shear force acting at point C Express your answer to three significant figures and include the appropriate units. Request Answer 6 ft μA Value C W Request Answer Units 6 ft Determine the internal moment acting at point C Express your answer to three significant figures and include the appropriate units. www ? B Units < 1 of 1 900 lb-ft-A beam luadet with dist ributed Load as in figure Determine the madimnm deflection and its pusifion EI= 16-7=2 Nm Go KN loo l/m 4.5 m RIThe overhang beam is subjected to the uniform distributed load having an intensity of w = 60 kN/m. (Figure 1) Figure -3 m B- 50 mm -3 m 100 mm 1 of 1 Part A Determine the maximum shear stress developed in the beam. Express your answer to three significant figures and include the appropriate units. Tmax = Provide Feedback μÅ Value Units ?
- The Flexor loading micrometer will be used to load the beam. Calculate the deflection required to bend the beam to the desired strain. Deflection in a cantilever beam b inches wide by t inches thick is: 4PL3 y = Ebt3 %3D (4) where: y= deflection (in), P= force, lbs, L= distance from clamp to loading micrometer (10.0 in), E = Young's modulus for aluminum (10.4E6 psi). %3D %3D Stress at the rosette is given by: Mc/ = 6Px (5) %3D bt2 where: x= the distance from the loading micrometer to the rosette centerline (9.0 in), and P, b and t are as defined above. Using equations (4) and (5) above, determine the deflection required to impose a 15 Kpsi stress in the beam at the gage rosette centerline. What force will be applied by the loading micrometer at 15Kpsi? Do your work in the space below.All I want to know is how to get the deflection equation. Please explain in as much detail as possible! DON'T SOLVE THE PROBLEM, this picture was taken from the answer key; solving this problem does me no good. All I want is to know where the 17qL4/24EI is coming from- Detrmia he tensile and Compresou stras for the beam shown in fig 160 mm lo wlm 20 m 20 mm 120 T = 97-6 mm le
- L by the double integeration method. E = 200 GPa , I = 20 X10ʻmm“, and L = 3.0 m._Extra points will be added if you also model it using RISA-2D software. Send me the model file, the deflected shape in a PDF file Compute the values of slope and deflection for the beam shown below at x = with the maximum deflection values, and a screenshot (image) for the deflection value at the pointL shown on the deflected shape. 350 KN/m 70 KN/m 400 KN.mQ1: The solid shaft shown in Figure 1 is subjected to a load F which is fluctuated from 0 to 500 N. The shaft is none rotating and made from AISI1035 cold rolled. The reliability is 90% and stress concentration factor K, = 1.5. b. Find the maximum deflection using singularity function methods D F 50 200 F 50 500 200 250 500 All dimensions are in mm Figure 1Part A A simply supported shaft is shown in the figure below. Assume the following data: a = 16 in, b = 18 in, l = 20 in, P = 1000 lb, Tmin=0 lb-in, Tmax=2000 lb-in. The steel shaft diameter is 1.75 in. Determine the maximum deflection in bending of the shaft shown in the figure. Express your answer in inches to three significant figures. Enter positive value if the deflection is upward and negative value if the deflection is downward. Submit Previous Answers Request Answer Part B ΗΠΙΑΣΦΗ * Incorrect; Try Again; 4 attempts remaining vec Omaz = Submit bearings are self-aligning so act as simple supports Determine the magnitude of the maximum deflection in torsion of the shaft shown in the figure. Express your answer in degrees to three significant figures. ΑΣΦΗ ΠΕ vec Previous Answers Request Answer ? in ?