Design of Compression Members Flashcards

(27 cards)

1
Q

The selection of an economical rolled shape to resist a given
compressive load is simple with the aid of the column load
tables.

A

Design

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2
Q

In some cases, the search may continue until the_______-shape
is found

A

lightest

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3
Q

For shapes not in the column load tables, a ______-
approach must be used.

A

trial-and-error

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4
Q

If a compression member is supported differently with respect
to each of its principal axes, the ________- will be
different for the two directions.

A

effective length

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5
Q

All compression members so far are treated as _______-.

A

pin-ended

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6
Q

Generally speaking, a______ or _____, condition is very difficult
to achieve, and unless some special provisions are made,
ordinary connections will usually closely approximate a ________ or _______.

A

rigid, or fixedhinge or
pin connection

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7
Q

_________ decreases with increasing KL/r, a column
will ________ in the direction corresponding to the largest
slenderness ratio

A

Column strength, buckle

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8
Q

Whenever possible, the designer should provide _______ for
the weak direction of a column

A

extra support

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9
Q

the _________– provided by the beams, or girders, at
the end of a column is a function of the rotational stiffnesses
of the members intersecting at the joint

A

rotational restraint

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10
Q

__________ depends on the ratio of column
stiffness to girder stiffness at each end of the member

A

effective length factor K

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11
Q

due to bending or
flexure about the axis with largest slenderness ratio; usually
the minor principal axis (with smallest r)

A

Flexural buckling

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12
Q

twisting about the longitudinal axis;
occur only with doubly symmetrical cross sections with very
slender elements; standard hot-rolled shapes not susceptible
but members built up from thin plate elements

A

Torsional buckling

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13
Q

member bends and twists
simultaneously; occur only with unsymmetrical cross sections
i.e. C, T, 2L and equal leg L and no axis of symmetry
(unequal leg L)

A

Flexural-torsional buckling

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14
Q

can be defined as the elastic
buckling stress corresponding to the controlling mode of failure,
whether flexural, torsional, or flexural-torsional

A

Fe

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15
Q

For__________ sections, Cw may be taken as
Iyho^2/4, where ho is the distance between flange centroids, in lieu of
a more precise analysis

A

doubly symmetric I-shaped

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16
Q

warping constant, mm6

17
Q

For ____ and ______, omit the term
with Cw when computing Fez and take xo as 0.

A

tees and double angles

18
Q

The need for a torsional buckling analysis of a _________ shape will be rare.

A

doubly
symmetrical

19
Q

________- can be used for double angles
and tees

A

column load tables

20
Q

Column load tables give two sets of values of the available
strength, one based on _______________ and
one based on_____________-

A

flexural buckling about the x-axis, flexural-torsional buckling about the y-axis

21
Q

For__________, the tables are not based on
flexural-torsional buckling theory, but on the provisions of
NSCP 505.5/AISC E5

A

single-angle members

22
Q

For _________-, no need to account for slender
compression elements (already been done) in using the column
load tables

A

unsymmetrical shapes

23
Q

_________ (rolled shapes) is the most common built-up
shape

24
Q

________- must ensure that the built-up member acts as a
unit

25
the modified slenderness ratio depends on the value of ______
a/ri
26
Ki = _____ for angles back-to-back Ki = ______ for channels back-to-back Ki = _______ for all other cases
0.50, 0.75, 0.86
27
column load tables for double angles are based on the use of________ or ________
welds or fully tightened bolts.