x Determin the design Compressive12-5 Strength of the Cross- sectionaColumn shown with unbracedlength kala= 35m, Kyly=2mA-118:75 I= 10872 Iy= 3799 J-247 8ae =4.13 c?J= 247-8%3DTu = 9.57 C5.746E=2-1x

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

Answered: x Determin the design Compressive 2-5…

x Determin the design Compressive 2-5 Strength of the Coss-sectional CGolumn shown with unbraced tength kala= 35m,kyly=em 3799 J= 247.8 2. e =4.13 a %3D A=118.75a I= 10872 Iy- a" %3D Tu=9.570 Deo3

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: Find the stresses in members BC BD and CF for the truss shown. Indicate the tension or compression.…

A: We will use method of joints

Q: -5 @ 3m-15m- C F H J K ML boo I A 4@4m=16m B D G E 60 kips A For the truss shown, what is the force…

Q: E Bars AB CD are rigid. The supports are pins at A and C and the Steel. What maximum force P can be…

A: Maximum force P

Q: Determine the required tension steel area for a rectangular beam with given properties below, d'…

A: Given d= 475mm Fy = 400 Mpa

Q: A 50 mm x 100 mm purlin is used for a roof truss. Spacing of trusses is 3.5 m Weight of roofing…

Q: 2-A teel pod is sfreteked between fwo rigid walls ard carries a tensile Coad f GO00N at C.f the…

Q: Problem 3 in the steel structure shown, a 6-mm-diamter pin is used at D and 10-mm-diameter pins are…

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: For the truss and loading shown, determine most economical cross-sectional area (in in2) of member…

Q: Problem 2: Determine the gross area of steel needed to design the bar force members at BC, BE, and…

A: To find area of bar AE, BE, BC

Q: Determine the smallest safe cross-sectional areas of members CD, CI and CH for the truss shown. The…

Q: M Deter MINE THE MAX Dez of the Beam

Q: For the plate shown, the distance d required to eliminate the flexural .effect at section a - a is…

A: True

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

Q: A PROB. 1.8-12 a 2P B (a) D XII Gusset plate Rivet (b) Section

Q: Problem 1: The rigid bar ABC is supported by AD and BE. Determine: a. Inclination of member ABC…

Q: Q. No. 4: An aluminium Z section has the dimensions shown in Figure Q. No.4. The yield strength…

Q: Determine the faces in members BD and DE GOKN A 120 KN 3m 120KN G 4m

A: Consider the section of the truss. Here, T is the tension and C is the compression.

Q: PART 2 : COMPUTE THE AXIAL STRESSES IN ALL MEMBERS OF THE TRUSS SHOWN. USE 300 sq. mm AND 250 sq. mm…

A: Question is based on truss supported on roller and hinged support. Span length of member and loading…

Q: show

Q: Knowing that P=(4a) kN, Tallow.=60 MPa, Oallow.compressive =140 MPa, a) Find the diameter (d) of the…

A: It is Given that, P = 42 KN ( as it is Mentioned in the Question) Allowable Tensile…

Q: Question 3. in the truss shown, a-5m, b 4m, and c=4 m Determine the force in member BE is kN. Use ve…

Q: 1. Is this truss (simple, compound or complex )truss? 2. Determine the bar force in member AF of the…

Q: 100KN 30° B с 120KN 6 D 60KN DETERMINE THE FORCES MEMBERS AB, FC, GF,

A: We have a truss structure.To find the force in members AB, FC, GF and GD-

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

Q: Given the truss and loading shown below, determine the stress at member FC if P₁ = 18.375 Kips and…

Q: composite shaft AC is made by shrink-fitting a titanium-alloy sleeve of length L3 = 4 ft over…

A: (a) Angle of Rotation at B (θB):Using the Displacement Method, we can calculate the angular…

Q: Members of the following 2-DOF beam system have the same El and length L C. Which of the following 4…

A: Since K12= K21 Hence Statement C and D are Correct Stiffness caused due to rotation such as K11and K…

Q: the

A: A device for measuring corneal thickness that is installed on a slit-lamp is known as pachometer. It…

Q: 15 Flad the ABE GO Kri CD = 70 ksi BC - 50 ksi 0.4 in2 4. 0.3 n? 4P- 3p P4

Q: ction is welded to a noc owing figure shows. De equired thickness, roun

Q: A=7 B=7 D=2 C=5 E=8 F=4 Change letters into numbers... Determine the total area (mm2 ) of the given…

A: step 1-

Q: One1 the are two For thickness Subjected ponts Subjected aN/m. is the retanglugar plate all…

A: To find - Equilibrium equation of the structure.

Q: 3. Use the charts to determine the reinforcing bars to be placed in its end faces, P-120k.P-212k M,…

A: Given f'c=5ksify=50ksiPL=120kipPD=212kipML=75kip-ftMD=145k-ftb=14''h=20''cover=2.5''

Q: The aluminum rod AB (Gal = 27 GPa) is bonded to the brass rod BD (Gbr = 39 GPa). The portion CD of…

Q: What is the Maximum Shear Stress, t, on the centric axially loaded member shown? The cross-sectional…

A: Given data : Axial load (P)=40 kipsCross sectional area (A)=2 in2

Q: Safe Support Spacing and S-1-bd Table below shows formulas for shear, bending moment and deflection…

A: Bending stress Equation , Shear stress Equation ,

Q: Is the beam cracked at service loads? The cracking moment is Mer Compute I, for the uncracked…

A: NOTE: Due to some technical error, you may find some difficulty in reading the symbols and formulas.…

Q: Q₁: Analyze the truss shown below B с D <50kw 3m EA is Constant 100 ku for all members +. Am X A Am

A: RA+RE=100kNRA×8-100×4-50×3=0RA=68.75kNRE=100-68.75=31.25kNHorizontal force ∑Fx=0HA-50=0HA=50 Zero…

Q: A sheet of copper is stretched bi-axially in the xy-plane. If the strains in the sheets are Ex=0.40…

Q: 1) Find the allwable safe loadpf fhe stresses in the ban are fhe followung BC - 50 ksi O.4 in2 ABE…

A: Given:- A composite bar of different cross-section is given The cross-sectional area of AB bar =…

Q: direction lead on the roof - 50%-2 (23) 3³/2/1/1000 =18.29 KN alculate Reaction support 1 22 Wisse 2…

Q: The rigid bar ABCD supports point loads at A and D and is being supported by two bars at B and C.…

Q: Cm 4m 4m Gom G Gm. F Gm 76 KN 14 76 KN

Q: solve the stresses in members DF,DG and EG using method of sections

A: Given data Using method of section

Q: Try to write out the stress boundary conditions of the cantilever beam. ( not include the fixed…

A: Three force are there on cantilever beam F force, UVL load and q force.....

Question

x Determin the design Compressive
12-5 Strength of the Cross- sectiona
Column shown with unbraced
length kala= 35m, Kyly=2m
A-118:75 I= 10872 Iy= 3799 J-247 8a
e =4.13 c
?
J= 247-8
%3D
Tu = 9.57 C
5.746
E=2-1x

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

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

Problem 3 & 4. For the following built up beams, calculate the shear flow q (lbs/in or kips/in) at the connection between the members that form the beam and indicate if the connection is adequate.
Determine the required tension steel area for a rectangular beam with given properties below, d' =75mm b = 350mm d = 470mm fc' = 30MPa fy = 400 MPa A. Mu = 470KN-m, As = mm2 B. Mu = 1000KN-m, As = mm2
2. Like 20 ft 3 KLF K 12000 Mmax= A max= 932 2adbl
A short prismatic member is subjected to load P- 100 kips at comer shown by Red Dot as shown in figure 02. Analyze the given section to (a) Develop fiber stress equation. (b) Locate the N.A. (c) Find the stress at all the comers. 344 12 3 15°
For the truss and loading shown, determine most economical cross-sectional area (in in2) of member DF, if P = 40453 lb, Q = 38513 Ib, y = 7.94 ft, and the stress in the member is 12.47 ksi . Round off the final answer to two decimal places. M 0004(1).png ... В E 4 panels at 10 ft = 40 ft
Please answer in written notes clear please. Here are the steps to solve 1) solve external reactions 2)cut the beam in sections for moment equations 3) use the double integration method (slope is 1 integration of moment & deflection is 2nd integration of moment) 4) find the boundary conditions (at A x=0, v(0)=0 v'(0)=0, at B x=L -> v(0) left = v(0) right & v'(0) left = v'(0) right, at C x=2L , v(0) left = v(0) right & v'(0) left = v'(0) right) use these conditions to plug into equations of slope & deflection to find constants 5) Max deflection & slope is either at B or D so plug into the slope & deflcetion equations x=L and x=3L
EQuiz No.3 584nkkz1 Cc7KLzOsdr9YUFgvcfFSqpsdlyljtewQ/formResponse Choose the correct answer What will be the value of load applied parallel to the diagonal of (100x100x100))mm cube since the splitting tensile strength=3 Mpa 57.8 KN O 46.7 KN O 47.1 KN O (28)=27.5 Mpa, then the fc(180)=-- for concrete produced using moist
determine the zero foce member for this please
check the stress in member BD, DE, and EG using method of sections
A steel beam is subjected to a uniform load with length of 8m. Assume that the beam is simply supported. Use Fy= 248 Mpa. Properties of W-shape beam d=229 mm bf=210 mm rf=23.7 mm Tu-14.50 mm kdes=33. 80mm ry=53.80 mm Ix=113 x 10^6 mm^4 Iy-36.9 x 10^6 mm^4 Sx-990 x 10^3 mm^3 Zx 1150 x 10^3 mm^3 J-2100 x 10^3 mm^4 Cu-387 x 10^9 mm^6 What is the nominal shear strength capacity of the section (in kN)?
The rigid bar ABCD supports point loads at A and D and is being supported by two bars at B and C. Determine the absolute values of the deformation at point A, B, C, D
X= 482 show complete solutions and FBD