The tee shape shown is used as a short post to support a load of P = 3700 lb. The cross-section includes a left-side flange (1) with dimensions bf x hf, and a stem (2) of dimensions tw x (d-tf). Assume L = 18 in., bf = 11.5 in., tf = 2.0 in., tw = 2.0 in. and d = 12.0 in. The load P is applied at a distance a = 3.5 in. from the surface of the flange. Determine the normal stresses at points H and K, which are located on section A-A. L P A H K X (1) H d x (2) K Cross section
The tee shape shown is used as a short post to support a load of P = 3700 lb. The cross-section includes a left-side flange (1) with dimensions bf x hf, and a stem (2) of dimensions tw x (d-tf). Assume L = 18 in., bf = 11.5 in., tf = 2.0 in., tw = 2.0 in. and d = 12.0 in. The load P is applied at a distance a = 3.5 in. from the surface of the flange. Determine the normal stresses at points H and K, which are located on section A-A. L P A H K X (1) H d x (2) K Cross section
Elements Of Electromagnetics
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ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
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
Transcribed Image Text:The tee shape shown is used as a short post to support a load of P = 3700 lb. The cross-section includes a left-side
flange (1) with dimensions bf x hf, and a stem (2) of dimensions tw x (d-tf). Assume L = 18 in., bf = 11.5 in., tf = 2.0 in.,
tw 2.0 in. and d = 12.0 in. The load P is applied at a distance a = 3.5 in. from the surface of the flange. Determine the
normal stresses at points H and K, which are located on section A-A.
=
L
A
H
K
Z
A
x
by
|(1)|
H
d
x (2)
K
Cross section
tw
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