. Given the isosceles triangle with a base b=10 and a height h=10 inches determine the plastic
modulus Z if Fy= 100 ksi
97.631
A box section is 8 times stronger than a wide flange section because
ALL ELEM. ARE STIFFENED
A stiffened element is more critical than an stiffened element in terms of local buckling
FALSE
when a section behaves in the plastic mode, the neutral axis divides the section into two
EQUAL AREAS
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 ratio to ensure that
THE ELEM. IS CAPABLE OF
LARGE STRAIN PRIOR TO LOCAL BUCKLING
The moment of inertia I of an isosceles triangle with respect to the centroid is
bh^3/36
The limit for the plastic moment Mp is
1.5My
Given the isosceles triangle with a base b=10 and a height h=10 inches determine the location
of its plastic centroid from the top
3.536
Main or primary flexural members are called
beams
Given the isosceles triangle with a base b=10 and a height h=10 inches determine the location
of its geometric centroid from the top
20/3
Lateral torsional buckling is primarily due to the lateral translation of the
COMPRESSION
FLANGE
Shape factor is simply a ratio of
EITHER OF THE TWO ABOVE
Given the isosceles triangle with a base b=10 and a height h=10 inches determine the section
modulus S if Fy= 100 ksi
83.333
Uniformly compressed elements have no compact limits
FALSE
. For a simply supported beam (pin ended ) with no transvere loads and with eqaual end
moments in single curvature, the value of Cb is
1.0
Beams with continuous lateral support such as those which carry continuous slab are said to
be
LATERALLY SUPPORTED
The factor that takes into account the non-uniform bending moment distribution over an
unbraced length Lb is
Cb
The yield strength of a material is based on the
UPPER YIELD POINT
Given the isosceles triangle with a base b=10 and a height h=10 inches determine the shape
factor if Fy= 100 ksi
1.172
. The moment of inertia I of an isosceles triangle with respect to its base is
bh^3/12
The value of Fr (residual stress) for welded built-up shapes in the old AISC code is
16.5
Flexurally compressed elements have no non-compact limits
T
For a simply supported beam (pin ended ) with no transverse loads and with eqaual end
moments in reverse curvature, the value of Cb is
1.32
d length Lb greater than that required are said to be
LATERALLY
UNSUPPORTED