Beam-Column Flashcards

1
Q

The value of Fr (residual stress) for welded built-up shapes in the old AISC code is

A

0.7Fy

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2
Q

For a simply supported beam (pin ended) with no transverse loads and with equal end moments in single curvature, the value of Cb is

A

1

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3
Q

For a simply supported beam (pin ended) with no transverse loads and with equal end moments in reverse curvature, the value of Cb is

A

1.32

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4
Q

The number of plastic hinge is determined by the degree of indeterminacy plus

A

1

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5
Q

A stiffened element is more critical than an unstiffened elements in terms of local buckling

A

True

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6
Q

A compact section satisfies the condition that the width to thickness ratio of a plate element shall not exceed the limit for width to thickness ration to ensure that

A

both

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7
Q

The limit for the plastic moment Mp is

A

1.5My

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8
Q

Flexurally compressed elements have no non-compact limits

A

False

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9
Q

A moment resisting frame or a beam-column frame is said to be braced if there is no

A

sidesways or lateral translation

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10
Q

A column is a part of an MRF. Determine the moment magnification factor B2 if the column is not braced against side sway. Note: The column is pinned at both ends and the end moments produces reverse curvature.

A

2.22

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11
Q

The interaction equation below is a

A

Linear

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12
Q

When a section behaves in the plastic mode, the neutral axis divides the section into two

A

Equal Areas

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13
Q

Perfectly plastic behavior means that the material will not rupture at a specified

A

Strain

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14
Q

In a beam-column a secondary moment is caused by the

A

primary deflection

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15
Q

The AISC value for Cm shown below is a modification which must always be

A

less than or equal to one

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16
Q

A column is a part of an MRF. Determine the moment magnification factor B1 if the column is braced against side sway. Note: The column is pinned at both ends and the end moments produces reverse curvature.

A

0.89

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17
Q

What is the relative stiffness of a fixed joint

A

0

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18
Q

The factor that takes into account the non-uniform bending moment distribution over an unbraced length Lb is

A

Cb

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19
Q

In a beam-column a primary moment is caused by the

A

primary loads

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20
Q

Moment magnification may not be required if second order analysis is used

A

True

21
Q

A member of structure is safe if the ration of the load P with the resistance R is less than or equal to

A

one

22
Q

The yield strength of a material is based on the

A

upper

23
Q

The range of values of the effective length factor k for sway frame is

A

1 < k < 20

24
Q

Shape factor is simply a ratio of

A

either

25
Q

A member subjected to some degree of bending and/or flexure is called

A

beam

26
Q

What is the relative stiffness of a roller joint (Note roller free to move laterally

A

infinity

27
Q

Cm = 1 is a conservative value for braced and unbraced frame

A

False

28
Q

A plastic moment is the largest moment which could be developed by the section

A

True

29
Q

What is the effective length factor k of a column fixed at one end and roller (free to move laterally) at the other end

A

2.0

30
Q

In the LRFD criteria for strength of flexural members, the main objective is to determine

A

Moment Capacity

31
Q

For a bearing stress concept, the bearing stress per bolt considers an area equivalent to the area of the

A

Hole diameter x thickness

32
Q

Bearing failure of the plate happens prior to shearing plate failure

A

False

33
Q

Minimum distance “Lc” and minimum ctc spacing “s” is used to prevent

A

Shearing of the bolt

34
Q

The transfer of loads from one plate to the other is basically through
with the plate side hole

A

Bearing

35
Q

The main difference between the bolt and rivet is in the

A

Method of tightening

36
Q

A length correction factor ofd ______
is applied to account for the effect of length connection

A

80%

37
Q

Which of the following type of connection permits a bolt to be snug tight

A

Slip critical type

38
Q

For a simple stress concept, the shear stress per bolt considers an area equivalent to the area of
the

A

Plane Section

39
Q

When hole elongation exceeds 25° is tolerated then shearing failure of the bolt is more likely to
happen.

A

True

40
Q

The actual proof load given on tables is based on

A

stress

41
Q

Maximum distance “Lc” and maximum ctc spacing “s” is used to prevent

A

Shearing of the bolt

42
Q

Pre-compression of the plates for a riveted connection is achieved by

A

Applying heat and pressure

43
Q

Slip critical connection is basically achieve by

A

Friction between plates

44
Q

When threads are included at the shear planes the nominal strength Rn of the bolts

A

Decrease

45
Q

When hole elongation exceeds 25° is tolerated then the connection is slip critical

A

True

46
Q

For a tension stress concept, the tension stress per bolt considers an area equivalent to the area of the

A

Bolt Section

47
Q

For a slip critical connection the failure mode of the bolt is by

A

Bearing

48
Q

Hole elongation is common to connection where the failure mode is by

A

Bearing of the plate