Answered: 1 m Ув 2 m C B 4 kN 3 m 0.5 m 6 kN D

Structural Analysis

6th Edition

ISBN:9781337630931

Author:KASSIMALI, Aslam.

Publisher:KASSIMALI, Aslam.

Chapter2: Loads On Structures

Section: Chapter Questions

Problem 1P

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■ Determine the maximum T of the structural arrangement as shown below (S275). T I 25 25 25 25 25 12 TYPICAL 20 mm THK PL 50 30 30 30 50 T
find out F, KN F23 f13 f16
Dimension the cross section of the rectangular cross section cantilever bar given loading status and dimensions. (Ostetx = 1200 N/cm²; Listetx = 180 N/cm) 4000N b . 4 N/cm h = 2b 400 cm
10 cm 3cm 3cm 2em 2cm 40 cm Center f wheel + ass of rotation 1. An 80 cm diameter metal wheel has the cross-section shown. Determine the centroid of the cross section area relative to O Determine the centroid of the cross section edge/outline relative to O
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Yo 3.5 3/4 1. The cross section shown in the figure is a structural member known as a z- section.Compute the following: (1) cross sectional area, (2) centroidal moment of inertia,lxo. And (3) centroidal moment of inertia, lyo. 2.625 6-4.5- 3/4 3/4 3/4 '1.375 3.5
The image below shows a beam subject to two couples, F₁ = 670 N and F2 = 760 N. (Figure 4) = = 1.40 m, 22 1.10 m, h = 0.12 m, 0 = 50°, and = 28°. The dimensions are 1 What is the net moment on the beam due to the two couples? Express your answer to three significant figures and Include the appropriate units.
For the given properties of the beam below, determine the safest wu that the beam will carry. bf = 850mm bw = 400mm tf = 100mm %3D d = 400mm d' = 100mm fc' = 34MPA fy = 400MPA As = 8-32mm bars %3D The answer is kN/m Pu bf キ 50 KN (Factore d) load Wu As t. A 5m + bw +
find the row of bm1 tp1 and tp2
i need the answer quickly
Convert the properties of your assigned AASHTO I-beams to Sl units. B1 BI Assigned AASHTO I-beam Туре 1 Туре 2 Group No. D2 1 D3 D2 2 D4 B3 B4 B5 Туре 3 Туре 4 Туре 5 Туре 6 B3 B4 4 DI B6 B6 D5 D6 DS Туре 1 Туре 2 8 B2 D6 Туре 1-IV Dimensions (inches) Type V-VI Туре D1 D2 D3 D4 D5 D6 B1 B2 B3 B4 B5 B6 28 4 3 5 5 12 16 6 3 5 II 36 3 6 6 12 18 6 3 6 III 45 4.5 7.5 7 16 22 7 4.5 7.5 IV 54 8. 6 8. 20 26 8 6. 9 V 63 4 10 8. 42 28 8 4 13 10 VI 72 5 3 4 10 8 42 28 8 4 13 10 Properties: Area in.? Inertia Ybottom in. Weight kip/ft Туре in. 276 12.59 22,750 0.287 II 369 15.83 50,980 0.384 III 560 20.27 125,390 0.583 IV 789 24.73 260,730 0.822 V 1,013 31.96 521,180 1.055 VI 1,085 36.38 733,320 1.13 67
Solve the differential equation for dy/dx = 4/x^2-1

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