Om ang g caT VI CIO nPPOTcd Uy ImI an U ports a 42 kips load at Point B (midway between Pin A and Roller C). at Pin A (0A), the deflection at Point B (AB), the slope at Point D C at Point D (AD). The beam has the following properties: E 10,00 42k 15FT 15r 12 FT er beam shown below has length L, and a fixed support at the left e niformly distributed load (w) at the free end. The distributed loa from the fixed end. Determine the formulas for formulas for 0 of the cantilever beam. [Note: Just like the formulas inside the function of w L a Eand I.1. +hese fo ues. he

Structural Analysis
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ISBN:9781337630931
Author:KASSIMALI, Aslam.
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Chapter2: Loads On Structures
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The 42 foot long overhanging beam shown is supported by a pin at A and a roller at C. The beam supports a point load of 42 kips at point B. Determine the slope at pin A, deflection at point B, and the slope and deflection at point D. Modulus of Elasticity, E = 10,000ksi, Moment of Inertia, I = 2500in4.

Let slope and deflection be functions of x, with x positive to the right.

Om ang g caT VI CIO nPPOTcd Uy ImI an U
ports a 42 kips load at Point B (midway between Pin A and Roller C).
at Pin A (0A), the deflection at Point B (AB), the slope at Point D C
at Point D (AD). The beam has the following properties: E 10,00
42k
15FT
15r
12 FT
er beam shown below has length L, and a fixed support at the left e
niformly distributed load (w) at the free end. The distributed loa
from the fixed end. Determine the formulas for formulas for 0
of the cantilever beam. [Note: Just like the formulas inside the
function of w L a Eand I.1.
+hese fo ues. he
Transcribed Image Text:Om ang g caT VI CIO nPPOTcd Uy ImI an U ports a 42 kips load at Point B (midway between Pin A and Roller C). at Pin A (0A), the deflection at Point B (AB), the slope at Point D C at Point D (AD). The beam has the following properties: E 10,00 42k 15FT 15r 12 FT er beam shown below has length L, and a fixed support at the left e niformly distributed load (w) at the free end. The distributed loa from the fixed end. Determine the formulas for formulas for 0 of the cantilever beam. [Note: Just like the formulas inside the function of w L a Eand I.1. +hese fo ues. he
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