6 in. Problem 2: The top plate made of 2014-16 aluminum is used to reinforce the...
A 20- ftft-long column is made of aluminum alloy 2014-T6.
If it is pinned at its top and bottom, and a compressive load PP
is applied at point AA, determine the maximum allowable magnitude
of PP using the equations
σallow=[54000(KL/r)2]σallow=[54000(KL/r)2] and
P/A(σa)allow+Mc/Ar2(σb)allowP/A(σa)allow+Mc/Ar2(σb)allow, with
(σb)allow(σb)allow = 22 ksiksi .
Express your answer to three significant figures and include
appropriate units.
Problem 13.118 11 of 21 A 20-ft-long column is made of aluminum alloy 2014-T6. A 5.25 in. 0.5 in. X x...
pls solve it right this time
Segment A of the composite beam is made from 2014-T6 aluminum alloy and segment B is A-36 steel The allowable bending stress for the aluminum and steel are (ơallow)al-15 ksi and (Ơallow),-22 ksi. Suppose that L-14.7 ft. (Figure 1) Part A Determine the maximum allowable intensity w of the uniform distributed load. Express your answer using three significant figures Figure 1 of 1 1.067 kip/ft Submit Incorrect; Try Again; 5 attempts remaining 3 in...
Segment B of the composite beam is made from aluminum (Es=70 GPa) and segment A is steel (Ext=210 GPa). The allowable bending stress (tensile/compressive) for aluminum and steel are allow)al=100Mpa and (allow)se=150MPa. Determine the maximum allowable intensity (w) of the uniformly distributed load. (Hint: NA is located at 150 mm from top edge. Show that I=850*10 mm. for aluminum equivalent). 100 mm W steel 100 mm 4.0 m 300 mm aluminum B
The cross-section of a beam is shown below. The top rectanular
piece of the cross-section is a steel section 6 inches wide by 8
inches deep. The dimensions of the member are shown below in the
table. The cross-section is loaded in bending by a moment about the
zz-axis. The allowable bending stress of the cross-section is 42
(ksi).
Determine:
a) the elastic centroid of the cross-section.
b) the yield moment.
c) the plastic centroid of the cross-section
d) the...
Problem 4. 6–165. The beam is made of elastic-perfectly plastic material. Determine the maximum elastic moment and the plastic moment that can be applied to the cross section. Take Ty = 36 ksi. 6 in. 1.5 in. 3 in. 1.5 in.
A beam with cross-section as shown in Figure 2(a) is made of an
elasto-plastic material. The stressstrain relationship of the
material is as shown in Figure 2(b): (a) A bending moment is
applied to this section and increased until the entire top flange
yielded. Calculate the magnitude of the moment at this stage of
loading. (b) Determine the yield moment of the beam (c) Determine
the ultimate moment capacity of the beam (d) Determine the shape
factor of the beam...
A wood beam (1) is reinforced on its lower surface by a steel
plate (2) as shown in the figure. Dimensions of the cross section
are b 1 = 220 mm , d = 385 mm , b 2 = 190 mm , and t = 25 mm . The
elastic moduli of the wood and steel are E 1 = 12.5 GPa and E 2 =
200 GPa , respectively. The allowable bending stresses of the wood
and steel...
The two 3-ft-long shafts are made of 2014-16 aluminum. Each has a diameter of 1.5 in. and they are connected using the gears fixed to their ends. Their other ends are attached to fixed supports at A and B. They are also supported by bearings at C and D, which allow free rotation of the shafts along their axes. (Figure 1) A torque of T=500 lb-ft is applied to the top gear as shown. Part A Determine the maximum shear...
Item 1 < 1 of 3 > Review Part A The composite beam is made of 6061-T6 aluminum (A) and C83400 red brass (B). If the height h= 40 mm, determine the maximum moment that can be applied to the beam if the allowable bending stress for the aluminum is (o allow = 122 MPa and for the brass (allowbr = 33 MPa. (Figure 1) Express your answer with the appropriate units. ? CH HÅR M = 4982.713 O a...
Q-1. You are testing a circular beam of two metals, 1045 steel and 2014-T6 aluminum, in a rotating-cantilever beam fatigue test. If you need to choose one of these metals so that you can essentially design a part made of that metal, and subject the part to a repetitive stress- amplitude without ever failing due to fatigue, which one would you choose (See the attached figure) 600 T-51-25 tanium alloy 500 00 Maximum 8 MP 300 Ductile Castro 200 700...