I= 940 in^4; E= 29050 ksi. Values for a= 9 and c= 7; please help!!
I= 940 in^4; E= 29050 ksi. Values for a= 9 and c= 7; please help!! Problem...
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copyable matlab code
The basic differential equation of the elastic curve for a cantilever beam as shown is given as: dx2 where E = the modulus of elasticity and I = the moment of inertia. Show how to use MATLAB ODE solvers to find the deflection of the beam. The following parameter values apply (make sure to do the conversion and use in as the Unit of Length in all calculations): E 30,000 ksi, 1 800 in4, P kips,...
PLEASE SOLVE USING MATLAB
The basic differential equation of the elastic curve for a cantilever beam as shown is given as 2 da2 where E = the modulus of elasticity and-the moment of inertia. Show how to use MATLAB ODE solvers to find the deflection of the beam. The following parameter values apply (make sure to do the conversion and use in as the Unit of Length in all calculations): E = 30,000 ksi, I = 800 in4, P-1 kips,...
Use Method of Virtual Work.
1. The 10 ft long steel (E = 29,000 ksi) cantilever beam shown below has a fixed support at the left end (Point A). The beam supports a 10 kips (downward) load at Point B and a 50 k-ft "point couple" (clockwise) at the free end of the cantilever (Point C). Region AB is 6 ft long with moment of inertia IAB = 500 in". Region BC is 4 ft long with moment of inertia...
2. The beam shown below supports three distinct HVAC units, one 1000 lb and two 500 lb. They are located at quarter points of the beam. If we say the moment of inertia is 1 = 400 in 4, and the Modulus of Elasticity is E = 29,000 ksi: a. What is the deflection of the beam at mid-span? b. Given an allowable deflection of L/240 (where L is the beam length in inches), is the deflection acceptable? 1000 lb...
Determine the maximum deflection (in inches) if the load is 16
kips. E = 29,000 ksi and I = 500 in4.
A B 6 ft- -6 ft-
16. Beam Deflection Using the method of progressive diagrams, find the centerline deflection for the given beam. Give the required values for each diagram (load, shear, moment slope(EI) and deflection) shown in the problem statement (see the pdf). 3 w 1 DATASET: 1 -2. Length A Length B Point Load P Uniform Load w Modulus of Elasticity Moment of Inertia 9 FT 10 FT 13 KIPS 1 KLF 29000 KSI 600 IN 4 -A- B- -- A - Correct Answer...
Material Modulus of Maximum Axial Maximum Shear Stress (o) Elasticity (E) Stress (t) Brass Steel Wood inum 10,500 ksi16 ksi 22 ksi 30 ksi 15,000 ksi 29,000 ksi 1,600 ksi 10 ksi 13 ksi 20 ksi 90 psi 1000 psi 2) A rectangular cantilever bearm is loaded by a moment Mo = 4500 ft-lbs at its end as shown below. The length of the beam is L 4 ft and the height of the beam is h 3 in. If...
Use the Principle of Virtual Work to determine the required value of I to limit the deflection at "B" of the beam shown below to 1.50 inches. For this beam, E- 4,000 ksi (note the change of the moment of inertia at B). Note that moment functions have been provided. 120 ft-kip B. 15' (31) 120 4.x Real Moments, M (ft-kip) 0 7.5 15- 2 Virtual Moments, m (ft) 0 E312 (STRUCTURAL ANALYSIS)
Hi, I need the solution to problem 4 ASAP. Thanks
Problem 3 (25 points): Adopting the methods you have learned in moment distribu- tion method. . (a) Evaluate the distribution factors for each span considering appropriate stiffness values. (b) Determine the fixed-end moments for each span. (c) Adopting the table that you have seen in class, determine the support moments at A B. and C. (d) Employing equilibrium equations for spans AB and BC, determine the remaining sup- port reactions...
A timber [E = 1,800 ksi] beam is loaded and supported
as shown. The cross section of the timber beam is b = 4
in. wide and h = 7 in. deep. The beam is supported at
B by a 0.875-in.-diameter aluminum [E = 10,500
ksi] rod, which has no load before the distributed load is applied
to the beam. After a distributed load of w = 610 lb/ft is
applied to the beam, determine
(a) the force carried by...