H.W1. The fixed end beam shown in fig(1),is loaded by a concentrated ultimate load 700kN.The beam has a total depth of 1000mm (effective depth of 930mm). Based on theACI318M code, find area of steel required for flexure at critical section .Usefc'=25MPA, fy=400MP..2. For beam shown in fig(2),if Wu=50kN/m, Pu=113KN, fc'=28MPa, fy=420MPA. Design beamfor flexure(use bar diameter=32mm).3. For cantilever beam shown in fig(3),if service live load=72kN/m, service dead load=30kN/m,fc'=23MPa, fy=350MPa.Design beam for flexure.Pu=113KNPu=113KNv Wu=50KN/300mm3.5m3.5m3.5mFig(2)Pu=700kN4m4m600mmFig(1)L.L=72KN/mD.L=30kN/mØ12mm3. 5m300mmFig(3)I am need all theseQuestionsuwo88500mm

As per Bartleby's guidelines we are supposed to answer only one question. Kindly repost other…

1. The fixed end beam shown in fig(1),is loaded by a concentrated ultimate load 700kN. The beam has a total depth of 1000mm (effective depth of 930mm). Based on the ACI318M code, find area of steel required for flexure at critical section .Use fc'=25MPa, fy=400MPA. FOL/. 1121 AT Col2 OMD f 12 OMD.

1. The fixed end beam shown in fig(1),is loaded by a concentrated ultimate load 700kN. The beam has a total depth of 1000mm (effective depth of 930mm). Based on the ACI318M code, find area of steel required for flexure at critical section .Use fc'=25MPa, fy=400MPA. FOL/. 1121 AT Col2 OMD f 12 OMD.

Structural Analysis

6th Edition

ISBN:9781337630931

Author:KASSIMALI, Aslam.

Publisher:KASSIMALI, Aslam.

Chapter2: Loads On Structures

Section: Chapter Questions

Problem 1P

See similar textbooks

Related questions

Q: Three bars at pinned at points A, B, and C as shown. The common joint, D, of these members is loaded…

Q: surrounded by a 304 stainless steel tube. Before the load is applied the gap between these two parts…

A: To find greatest axial load P Ebr=101GPa Est=193GPa

Q: V 6-3 A beam with an overhang is supported and loaded as shown in the figure. The beam is made of a…

A: Beam: Channel section: No. 14 b steel channel To find: The maximum tensile and compressive stress…

Q: The internal force in member AB is most nearly. 500 lb B 500 lb ↓ 4 ft 2 ft T -5-10 2 ft $ PD

Q: Q: Verify that the steel seetion W12 x 106 can be used for the cantilever beam shown in the Figure.…

A: The deflection in the beam is a horizontal member of the building or structure which goes under…

Q: Problem 912 Compute the stresses at A and B on the link loaded as shown in Figure P-912 if P = 9000…

A: a ) P = 9000 lb and F = 3000 lb Compute the stresses at A and B ? Solid mechanics problem.

Q: NS 5 ft iG B 920 lb 1145 lb 1760 lb -20 ft20 ft 20 t 20 -20120 t-

A: To find the force in member CD , ND and NK -

Q: A-1: In the previous part of this assignment, you were asked to find the size and depth of the FT3…

A: Following are the given information. Dimension of footing =6'×6'×1' 6" No of footing =8 Working…

Q: A tensile member consists of 2 ? 4 x 3 x 1/2 carries a service dead load of 50 k and live load of…

Q: As shown in Fig., Six bolts are used in the connection between the axial member and the support. The…

A: To find the diameter of bolt (d)-

Q: Draw the FDBS of member ADB and BEC 1m 1m B Oc E 1 m D 1.6 m A

Q: For the truss loaded as shown, calculate the axial stress developed in members CD, ND and NK. Use…

A: To find stress in NKND,CD

Q: From the figure below, determine member BD

A: Force in the vertical direction - RA + RC = 0 Sum of the moment at the point C- ∑MC = 0⇒-RA×8 +…

Q: = AT beam supports the three concentrated loads shown in Fig. P-556. N.A. is 3.5 in., INA- 97.0 inf.…

A: Given: P=1600 lbsy=3.5 inINA=97 in4

Q: For the beam with the cross-section shown and loads as follows: w-2 kN/m, M-4 kN-mand PkN, P-5.XY…

Q: Assuming A36 steel, select the most economical W8 section. Check the shear stress, and determine the…

Q: snip

A: The factored axis load is Pu=1.6×28=44.8kipsthe factored transversed load and bending moment…

Q: Q1 Delermine the design (ultimate) bending mement for the beam sections showen belowi- 300 mm 460 mn…

A: My dear, width of beam is given. effective depth of beam. effective cover is provided. area of 1 bar…

Q: Auniform bar 1 is connected to a tapered rod 2. Both are subjected to axial loads as shown. If P-7…

A: Determine the axial deformation of uniform bar 1 in mm

Q: The steel pipe is filled with brass and subjected to a torsion T-34kNm. Determine each torsion value…

A: T = 34 kN- m = 34000 NLength L = 100 cmDiameter of brass db = 4 cm = 0.04 mOuter dia of steel do =…

Q: A W610 x 82 beam of A 36 steel has end reaction of 302 kN and is supported on a plate with a length…

A: Yield Strength : Yield strength of an element is a maximum stress an element or component can bear…

Q: 3#9 12" 21" 3" tc = 4 ksi Grade 60 steel. NWC. M = 60 ft-k The sectim is cracked Computer the…

Q: Find the axia) stresses of member BD,CD,CE and state if it'is tensile or Compressive. Lf the avesses…

A: Method of section - Equilibrium of section of a truss is considered in method of section. An…

Q: Check the slenderness of the steel section against Local Buckling.

A: We know that for flexure sections are classified as compact, non compact and slender sections For a…

Q: A W14X120 is used as a tension member in atruss. The flanges of the member are connected to a gusset…

A: The order of the steel cross sections relies upon the heap that the part can convey prior to…

Q: predict the maximum stress and deflection in the simply-supported aluminum beam shown below, with h…

A: Given, h = 1 in, b = 10 in, L = 4 ft = 48 in P = 5 psi. Moment of inertia (I)I = bd312I = 10×1312I…

Q: nd the stress of each 14 members and identify whether each member is a compression or tension. The…

A: Assumption: Loads in downward direction is positive. Forces in upward direction is positive.…

Q: x Determin the design Compressive 2-5 Strength of the Coss-sectional CGolumn shown with unbraced…

A: Given:- The unbraced length of the column = KxLx = 3.5 m The unbraced length of the column = KyLy =…

Q: 4.5) The live load deflection d, is A) 1.331 in B) 1.112 in C) 0.620 in D) 0.434 in

Q: A W14X120 is used as a tension member in atruss. The flanges of the member are connected to a gusset…

A: Given: Section = W 14 x 120 fy=36 ksi fu=58 ksi Ag = 35.30 in2 tf = 0.94 in To find: The yielding…

Q: 4.4) The design shear strength D,V, is A) 81.1 kips B) 482 kips C) 529 kips D) 567 kips

Q: Detemine the magnitude of the average normal stress in member AB when T,35C Express your answer to…

A: This problem is related to stress and strain theory from strength of material. In this problem given…

Q: Design all Tension members of the truss. Use A36 steel type. Dead Loads and Live loads are shown in…

Q: Home work Q1/ steel bar of rectangular secton 5cm by the 16 cm carries an axial load of 50 kn.…

A: As per guidelines please post Q 2 separately

Q: H HAVANIS 160kN 140KN 120KN 10.8m 8.1m D = 100KN 130kN 150KN 8 panels @ 6m ea. = 48m Determine the…

Q: A W14X120 is used as a tension member in atruss. The flanges of the member are connected to a gusset…

A: The order of the steel cross sections relies upon the heap that the part can convey prior to…

Q: 13 lb, y = 7.94 ft, and the stress in the member is 12.47 ksi . Round off the final answer to two…

Q: A beam is built-up from the following A36 plates: 420x20 plates as flanges and 500x20 plate as web.…

A: Answer We are given that the beam span = 4 m and it is braced at the ends only means we get…

Q: Result Reviewer VI. Knowing that for the beam shown. The allowable stress is 80 kPa in tension and…

Q: Please show solutions on how to get the 2 value. The circle green in the figure. Civil engineering-…

A: Thickness of gusset plate, SectionA36 steel.Length of weld on one side, Welding done on three…

Q: 4.3) The design moment strength M, is A) 880 ft-kips B) 887 ft-kips C) 1038 ft-kips D) 934 ft-kips…

Q: 25. Design stress is less than the ultimate strength. Truo

A: (25)Design stress is the maximum allowable stress that a material can withstand under normal…

Q: Using method of sections, determine the members BD, CD, and CE. statics of rigid bodies

A: Given:- Given Data:Load at C=5kNLoad at E=10kips=44.5kNspan= 9mH=5m To find:- Force in member BD,…

Question

H.W
1. The fixed end beam shown in fig(1),is loaded by a concentrated ultimate load 700kN.
The beam has a total depth of 1000mm (effective depth of 930mm). Based on the
ACI318M code, find area of steel required for flexure at critical section .Use
fc'=25MPA, fy=400MP..
2. For beam shown in fig(2),if Wu=50kN/m, Pu=113KN, fc'=28MPa, fy=420MPA. Design beam
for flexure(use bar diameter=32mm).
3. For cantilever beam shown in fig(3),if service live load=72kN/m, service dead load=30kN/m,
fc'=23MPa, fy=350MPa.Design beam for flexure.
Pu=113KN
Pu=113KN
v Wu=50KN/
300mm
3.5m
3.5m
3.5m
Fig(2)
Pu=700kN
4m
4m
600mm
Fig(1)
L.L=72KN/m
D.L=30kN/m
Ø12mm
3. 5m
300mm
Fig(3)
I am need all these
Questions
uwo88
500mm

Expert Solution

This question has been solved!

Explore an expertly crafted, step-by-step solution for a thorough understanding of key concepts.

SEE SOLUTION Check out a sample Q&A here

Step 1

VIEW

Step 2

VIEW

Step 3

VIEW

Step by step

Solved in 3 steps with 2 images

SEE SOLUTION Check out a sample Q&A here

Knowledge Booster

Learn more about

Need a deep-dive on the concept behind this application? Look no further. Learn more about this topic, civil-engineering and related others by exploring similar questions and additional content below.

Similar questions

please solve part 4.1
DETERMINE THE THE IS MAXIMUM SAFE SERVICE LIVE LOAD THAT THE BEAM CAN CAN CARRY IF SERVICE DEAD L O A D THE BEAM WEIGHT OF THE BEAM SECTION fy = 415 MPa. TOP BARS BOTTOM BARS ARE CENTER DISTANCE 12 KM/M INCLUDING AND BASED ON THE CAPACITY SHOWN. fc : 40 MPa AND ARE 6-32 mm. AND ARE - 3 - 28 mm. CENTER TO 3 BETWEEN THE USE 2015 NSCP Is 108 mm 00 0 0 300 G ט1 108 352 70. A (1 7.2m B TOP BAR LAYERS ↓ 6.7M C OM
In steel design use nscp 2015 i need a complete solutions ty..
Find the stresses in A, B and C? 14-d Vem 14 6m 0.006 MN 0 cm B -HA- 4 IX 6em H
Determine the smallest allowable diameter for a circular cross-sectional area of members BD, BE and CE of the truss shown. The working normal stresses are 2000 psi in tension and 1200 psi in compression. (A reduced stress in compression is specified to reduce the danger of buckling.) 12 t 40 kips
Question # 1: Determine the force in each member of the truss and state if the members are in tension or compression. 300 lb 600 15 B 60015 GOO G 11. 244in. 6 ft load at point B, D, F = 600 lb load at pount A and H=300 lb distance AC = CE =EG = GH = 8FT -80---SA- [Answer: FAB=15001b-C. Fac-12001b-T, Fac0, For-12001b-T, Fan+ 12001b-C, F₁-601b-C. Form 721h-T, Use symmetry to obtain the rest of the members]
Principle of superposition The beam is indeterminate to the first degree. Force in member BD is chosen as the redundant. This member is therefore sectioned to eliminate its capacity to sustain a force. 60 kN/m 3 m 1.8 m 60 45 actual structure (a) 160 kN/m B FaD redundant рrimary structure ARD FRp applied Fap D
Q.2. The rigid bar AB, atrached to two verti cal rods as shown in Fig (e), is horizontal before the lead p is applied. If the load pe so kN, ditermine its Vertical mmovement. Aluminum Steel A300 mm 200 G A500 mm R-70 GN -3m- Fig (2)
Q1: A circular steel rod ABCD is loaded as shown below. Use the following data to Find the maximum stress and the deformation (AL) of the rod. Take E = 200 L3=1350 GPa. L2=2150 A L1 E Dia. 1 L1=1350 Р3-25 P1 L2 Dia. 2 P2=40 P2 P1=105 Dia2=45 L3 P3 D D 35 mm o Dia1=60
Check the slenderness of the steel section against Local Buckling. 340 mm Use Fy = 800 MPa. O Compact Slender I O Adequate 400 mm None of the choices 30 mm 20 mm 20 mm
Question 5: (Use a W12 section) Use A992 steel and select a W shape. a. Use LRFD. b. Use ASD. D= 340 kips L=670 kips 10' 35' 15' 10' Strong axis Weak axis FIGURE P4.7-5
Find the allowable bending stress for the following shapes. Assume adequate lateral support for the compression flange. a.) W30 x132 of A36 Steel