MTE Flashcards

1
Q

The actual rupture strength of a plastic material is greater than the ultimate tensile strength if we consider the reduce area due to

A

Necking

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
2
Q

Values for factor of safety in ASD is based on

A

All of the Above

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
3
Q

Strain hardening is the result of dislocation or ____________ of the metal crystals.

A

Movement

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
4
Q

LRFD is limited to inelastic behaviour

A

True

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
5
Q

Strength Limit State is to collapse prevention as Serviceability Limit State is to

A

Function

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
6
Q

Which of the following statement represents failure

A

NOTA

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
7
Q

ASD differ primarily with LRFD in providing

A

Safety Factors

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
8
Q

ASD is all about allowable stresses

A

True

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
9
Q

What is the factor of safety for Tension Members in LRFD considering the combination U=1.4D

A

1.56

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
10
Q

For high strength steel the plastic strain increases because of the increase on the ultimate strength

A

False

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
11
Q

The limit state is the dividing between failure and

A

Survival

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
12
Q

LRFD is all about allowable loads

A

False

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
13
Q

Reliability index is the number of times the measure of the variance is to the mean from the origin

A

False

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
14
Q

By how many percent is LRFD cheaper for a Tension Member Design compared to ASD if L/D=1

A

6%

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
15
Q

In ASD the values of the coefficient on the Load Combinations are not based on probabilities.

A

True

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
16
Q

Flexural Torsional Buckling is more commonly known as ___________ in beams

A

lateral torsional buckling, lateral-torsional buckling

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
17
Q

Cc is a dimensionless parameter for slenderness in ASD (T/F)

A

T

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
18
Q

Flexural buckling limit states includes elastic, inelastic and

A

Yielding

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
19
Q

When the actual width to thickness ratio is less than the limiting value set forth on the code,
then the column will not experience ___________________________

A

Local Buckling

20
Q

Given: Fy=100ksi
Determine the slenderness ratio kl/r when Fcr=(2/3)Fy at the end of pure elastic stage

A

65.5

21
Q

How many stiffened section does a HSS rectangular section has?

A

4

22
Q

The slender limits for stiffened element local buckling is always greater than the slenderness limits for unstiffened local buckling. (T/F)

A

T

23
Q

Which of the shapes is more vulnerable to lateral-torsional buckling?

A

unequal angle

24
Q

Slenderness ratio is measured by dividing ______________ over radius of gyration

A

effective length

25
Q

Shanley concept introduces the critical load at which buckling begins and this is less the critical load of Engesser. (T/F)

A

F

26
Q

The reason for a transition curve in between the elastic and plastic stage for a column behavior is mainly attributed to

A

Residual Stress

27
Q

Residual stress are compressive where the rate of cooling is fast. (T/F)

A

T

28
Q

Given: See Figure Question 11. Fy=100ksi
Determine the slenderness ratio kl/r when all the fibers become plastic.

A

18.9

29
Q

The limiting width to thickness ratio λr of a plate element subject to compression force is called

A

non-compact limit

30
Q

How many unstiffened element does a wide flange section has?

A

4

31
Q

Flame cutting of steel plates introduces compressive stresses at the points of cutting. (T/F)

A

F

32
Q

Given: See Figure Question 11. Fy=100ksi
What is the value of tangent modulus at the transition stage

A

(1/8)E

33
Q

Shape factors Q for slender elements is less than 1 while shape factors Q for non-slender elements is ___________

A

equal to 1

34
Q

Weak axis buckling is critical for columns under

A

axial compressive only

35
Q

Given: See Figure Question 11. Fy=100ksi
Determine the slenderness ratio kl/r if there where no residual stress.

A

53.5

36
Q

How many number of support does an unstiffened element has which makes it less stable than a stiffened element.

A

1

37
Q

Built up shapes are more stable than rolled shapes in terms of local buckling.

A

False

38
Q

For local buckling failure on columns, the element subject to local loads must experience

A

uniform compression

39
Q

The local shape factor Qs for is based on average stress developed in the plate element while the local shape factor Qa is based on ___________________

A

effective area

40
Q

λc is a dimensionless parameter representing the LRFD parameter for

A

slenderness

41
Q

Given: See Figure Question 11. Fy=100ksi
Determine the slenderness ratio kl/r when Fcr=(2/3)Fy at the elasto plastic stage.

A

23.2

42
Q

Residual stresses are tensile at the joints but not at the free end. (T/F)

A

T

43
Q

The point of load application at which no torsional behavior is induced in the member is called

A

NOTA

44
Q

Inelastic column buckling is common for long, slender columns. (T/F)

A

F

45
Q

Which of the shapes is more vulnerable to pure torsion?

A

Cruciform