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51.

What is stress concentration factor?(a) ratio of average stress to maximum elastic stress(b) product of average stress and maximum elastic stress(c) ratio of maximum elastic stress to average stress(d) twice the average stressI had been asked this question in an interview for job.This is a very interesting question from Modes of Failure, Slenderness Ratio and displacement topic in chapter Design of Tension Members of Design of Steel Structures

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52.

The tensile stress adjacent to hole will be ____________(a) about five times the average stress on the net area(b) about half the average stress on the net area(c) equal to average stress on the net area(d) about two to three times the average stress on the net areaI got this question during an online exam.The origin of the question is Modes of Failure, Slenderness Ratio and displacement topic in section Design of Tension Members of Design of Steel Structures

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Correct choice is (d) about two to three TIMES the average stress on the net area

The best explanation: From the theory of elasticity, the tensile stress adjacent to HOLE will be about two to three times the average stress on the net area, depending upon the ratio of diameter of hole to the width of plate normal to DIRECTION of stress.

53.

What is net section rupture failure?(a) rupture of member when the cross section reaches yield stress(b) rupture of member when the cross section reaches ultimate stress(c) rupture of member when the cross section reaches less value than yield stress(d) rupture of member when the cross section is reachesvery less value than ultimate stressThis question was addressed to me by my college professor while I was bunking the class.The question is from Modes of Failure, Slenderness Ratio and displacement topic in section Design of Tension Members of Design of Steel Structures

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Correct answer is (b) rupture of member when the cross section reaches ultimate stress

The best I can explain: The point adjacent to hole reaches yield stress FIRST when tension member with hole is loaded statically. The stress at that point remains CONSTANT and each fibre AWAY from hole progressively reaches yield stress on further loading. With increasing LOAD, deformations continue until finally rupture of member occurs when ENTIRE net cross section of member reaches ultimate stress.

54.

What is gross section yielding?(a) considerable deformation of the member in longitudinal direction may take place before it fractures, making the structure unserviceable(b) considerable deformation of the member in longitudinal direction may take place before it fractures, making the structure serviceable(c) considerable deformation of the member in lateral direction may take place before it fractures, making the structure unserviceable(d) considerable deformation of the member in lateral direction may take place before it fractures, making the structure serviceableThe question was posed to me in an interview.I'd like to ask this question from Modes of Failure, Slenderness Ratio and displacement in section Design of Tension Members of Design of Steel Structures

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The correct option is (a) considerable deformation of the member in longitudinal direction MAY take place before it fractures, making the structure UNSERVICEABLE

Explanation: Tension member without bolt HOLES can resist LOADS up to ultimate load without failure. But such a member will deform in longitudinal direction considerably(10-15% of its ORIGINAL length)before fracture and the structure becomes unserviceable.

55.

The displacement of tension member under service load is given by(a) PLEAg(b) PLE/Ag(c) PL/EAg(d) P/LEAgI got this question by my college professor while I was bunking the class.This intriguing question comes from Modes of Failure, Slenderness Ratio and displacement in section Design of Tension Members of Design of Steel Structures

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Right choice is (c) PL/EAg

The best EXPLANATION: The displacement, that is increase in length of tension MEMBER, under service load is given by Δ = PL/EAg, where Δ = Elongation of member in mm, P= unfactored axial load in N, L = length of member in mm, E = elastic modulus = 2×10^5MPa, AG = GROSS cross sectional AREA of member in mm^2.

56.

What is the maximum effective slenderness ratio for members always in tension?(a) 400(b) 200(c) 350(d) 150The question was asked in an online interview.My question is from Modes of Failure, Slenderness Ratio and displacement topic in portion Design of Tension Members of Design of Steel Structures

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The correct answer is (a) 400

To elaborate: The maximum effective SLENDERNESS RATIO for members always in tension other than pre-tensioned members is 400.

57.

The limits specified for slenderness ratio are not(a) applicable to cables(b) applicable to angle sections(c) applicable to built-up sections(d) applicable to circular sectionsI have been asked this question at a job interview.Asked question is from Modes of Failure, Slenderness Ratio and displacement topic in section Design of Tension Members of Design of Steel Structures

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Correct OPTION is (a) applicable to cables

To elaborate: The LIMITS SPECIFIED for SLENDERNESS ratio in the IS code are not applicable to cables. They are applicable to angle sections, built-up sections, circular sections.

58.

What is the maximum effective slenderness ratio for a member normally acting as a tie in roof truss or a bracing member?(a) 180(b) 200(c) 350(d) 400This question was addressed to me in my homework.My doubt stems from Modes of Failure, Slenderness Ratio and displacement in chapter Design of Tension Members of Design of Steel Structures

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Right option is (c) 350

Explanation: The maximum effective slenderness ratio for a MEMBER NORMALLY acting as a tie in roof TRUSS or a bracing member, which is not considered when subject to stress reversal resulting from action of wind or EARTHQUAKE forces is 350.

59.

What is the maximum effective slenderness ratio for a member subjected to compressive forces resulting only from combination of wind/earthquake actions?(a) 180(b) 200(c) 340(d) 250This question was addressed to me in unit test.Enquiry is from Modes of Failure, Slenderness Ratio and displacement in portion Design of Tension Members of Design of Steel Structures

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Correct option is (d) 250

To EXPLAIN: The maximum EFFECTIVE slenderness RATIO for a member subjected to compressive forces resulting only from combination of wind or earthquake actions, such that the deformation of such member does not adversely AFFECT stresses in any part of STRUCTURE is 250.

60.

What is the maximum effective slenderness ratio for a tension member in which stress reversal occurs?(a) 180(b) 200(c) 280(d) 300I had been asked this question by my school principal while I was bunking the class.Question is taken from Modes of Failure, Slenderness Ratio and displacement topic in division Design of Tension Members of Design of Steel Structures

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Right choice is (a) 180

The best explanation: The MAXIMUM EFFECTIVE slenderness RATIO for a tension member in which stress reversal OCCURS due to LOADS other than wind or seismic forces is 180.

61.

What is slenderness ratio of a tension member?(a) ratio of its least radius of gyration to its unsupported length(b) ratio of its unsupported length to its least radius of gyration(c) ratio of its maximum radius of gyration to its unsupported length(d) ratio of its unsupported length to its maximum radius of gyrationThe question was asked in quiz.Question is from Modes of Failure, Slenderness Ratio and displacement topic in section Design of Tension Members of Design of Steel Structures

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Right option is (b) ratio of its unsupported LENGTH to its least radius of gyration

The EXPLANATION is: Slenderness ratio of tension member is ratio of its unsupported length to its least radius of gyration. This LIMITING slenderness ratio is REQUIRED in ORDER to prevent undesirable lateral movement or excessive vibration.

62.

Which of the following is true about built up section?(a) Built up members are less rigid than single rolled section(b) Single rolled section are formed to meet required area which cannot be provided by built up members(c) Built up members can be made sufficiently stiff(d) Built up sections are not desirable when stress reversal occursThis question was addressed to me in a job interview.I need to ask this question from Tension Members and their Types in division Design of Tension Members of Design of Steel Structures

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The CORRECT answer is (c) Built up members can be made SUFFICIENTLY stiff

The best explanation: Built-up members, made up of two or more plates or shapes and connected to act as single member, are formed primarily to meet required area which cannot be provided by single ROLLED section. Built up members are more rigid because for same area much greater moment of inertia can be obtained than single rolled section. Built up members can be made sufficiently stiff to carry COMPRESSION and tension thus desirable when STRESS reversal occurs.

63.

Which of the following statement is correct?(a) angles placed on same side of gusset plate produce eccentricity about one plane only(b) angles placed on same side of gusset plate produce eccentricity about two planes(c) angles placed on opposite side of gusset plate produce eccentricity about one plane only(d) angles placed on opposite side of gusset plate produce eccentricity about two planesThis question was addressed to me at a job interview.This question is from Tension Members and their Types topic in chapter Design of Tension Members of Design of Steel Structures

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The correct choice is (a) ANGLES placed on same side of GUSSET plate PRODUCE eccentricity about one plane only

To elaborate: TWO angle SECTIONS can either be placed back-to-back on the same side of gusset plate, or back-to-back on the opposite side of gusset plate. When angles are connected on the same side of gusset plate, the eccentricity is about one plane only, which can be almost eliminated when the same angles are connected on opposite side of gusset plate.

64.

Which among the following comparison between angle and flat bars is not true?(a) for light loads, angles are preferred over flat bars(b) flat bar tension members tend to vibrate during passage of load in light bridges(c) flat bars are used instead of angles in case of stress reversal(d) angles are used instead of flat bars in case of stress reversalThe question was posed to me in homework.The above asked question is from Tension Members and their Types in division Design of Tension Members of Design of Steel Structures

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Right answer is (c) flat bars are used instead of angles in case of stress reversal

The best EXPLANATION: For light loads, angles are preferred over flat bars. In many light BRIDGES, flat bar tension MEMBERS tend to vibrate during passage of load. In case of stress reversal angles are more suitable whereas flat bars are unfit to carry compressive load on reversal due to their SMALL radius of gyration in one direction.

65.

Which of the following type of tension member is not mainly used in modern practice?(a) open section such as angles(b) flat bars(c) double angles(d) circular sectionThe question was posed to me in unit test.This is a very interesting question from Tension Members and their Types in division Design of Tension Members of Design of Steel Structures

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The correct answer is (b) flat bars

Explanation: Tension members were generally made of flat bars earlier. But modern practice is to use MAINLY the FOLLOWING sections for tension members: (i)OPEN sections such as angles, channels and I-sections, (ii)compound and built up sections such as double angle and double channels with or WITHOUT additional plates, (iii)closed sections such as circular, square, rectangular or HOLLOW sections.

66.

Bars and rods are not used as :(a) tension members in bracing systems(b) friction resistant members(c) sag rods to support purlin(d) to support girts in industrial buildingsThe question was asked by my school teacher while I was bunking the class.I want to ask this question from Tension Members and their Types topic in portion Design of Tension Members of Design of Steel Structures

Answer» RIGHT answer is (B) friction resistant MEMBERS

Easy explanation: Bars and rods are used as tension members in bracing systems, sag rods to support purlin between trusses, to support girts in INDUSTRIAL buildings, where light structure is desirable. Rods are also used in arches to resist thrust of ARCH.
67.

Sagging of members by built up bars and rods may be minimised by(a) increasing length diameter(b) increasing thickness ratio(c) fabricating rod/bar short of its required theoretical length(d) fabricating rod/bar more than its required theoretical lengthI have been asked this question in examination.This intriguing question comes from Tension Members and their Types in section Design of Tension Members of Design of Steel Structures

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The correct choice is (c) fabricating rod/bar short of its required THEORETICAL length

Explanation: Sagging of members by built up BARS and rods may be minimised by limiting length DIAMETER or THICKNESS ratio or by fabricating the rod/bar short of its required theoretical length by some arbitrary amount and drawing into place to provide an initial TENSION. The same effect may be produced by providing turnbuckle in the rod.

68.

Which of the following statement is not correct?(a) Cables in form of wires ropes and strands are used in application where high strength is required(b) Cables are generally long and their flexural rigidity is negligible(c) They are flexible(d) They are recommended in bracing systemsI got this question in class test.My enquiry is from Tension Members and their Types topic in portion Design of Tension Members of Design of Steel Structures

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Correct CHOICE is (d) They are recommended in BRACING systems

To explain I would say: CABLES used as floor suspenders in suspension bridges are MADE from individual strands wound together in rope like fashion. Cables in form of wires ropes and strands are used in application where high strength is required and flexural RIGIDITY is unimportant. Cables are generally long and their flexural rigidity is negligible. They are flexible. They are not recommended in bracing systems as they cannot resist compression.

69.

Which of the following statement is correct?(a) single angle section with bolted connection produce eccentricity about both planes(b) single angle section with bolted connection produce eccentricity about one plane only(c) single angle section with welded connection produce eccentricity about both planes(d) single angle section with welded connection does not produce eccentricity about one planeThis question was addressed to me in an online interview.The doubt is from Tension Members and their Types in section Design of Tension Members of Design of Steel Structures

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Correct option is (a) single angle section with BOLTED connection produce eccentricity about both planes

Easy EXPLANATION: Single angle section with bolted connection produce eccentricity about both planes, whereas single angle section with welded connection may produce eccentricity about ONE PLANE only.

70.

The strength of tensile members is not influenced by :(a) length of connection(b) net area of cross section(c) type of fabrication(d) length of plateI got this question in homework.The origin of the question is Tension Members and their Types topic in section Design of Tension Members of Design of Steel Structures

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Correct answer is (d) length of plate

Easiest explanation: The strength of tensile members is influenced by factors such as length of connection, size and spacing of FASTENERS, size and spacing of fasteners, NET area of CROSS section, type of fabrication, connection eccentricity, and shear lag at the END connection.

71.

What are steel tension members?(a) Structural elements that are subjected to direct compressive loads(b) Structural elements that are subjected to direct tensile loads(c) Structural elements that are subjected to indirect compressive loads(d) Structural elements that are subjected to indirect tensile loadsI got this question in an international level competition.I'd like to ask this question from Tension Members and their Types in chapter Design of Tension Members of Design of Steel Structures

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Right OPTION is (b) STRUCTURAL elements that are subjected to direct tensile loads

For explanation: Steel tension members are those structural elements that are subjected to direct axial tensile loads, which tend to ELONGATE the members. A member in PURE tension can be stressed up to and beyond the yield limit and does not buckle LOCALLY or overall.