The cross-sectional dimensions of the beam shown in the figure are a = 4.2 in., b = 5.5 in., d = 4.5 in., and t = 0.33 in. The internal bending moment about the z centroidal axis is M, = -4.15 kip-ft. Determine (a) the maximum tension bending stress (a positive number) in the beam. (b) the maximum compression bending stress (a negative number) in the beam. b (typ.) a a Answers: (a) OmaxT psi (b) Omax C = psi

The cross-sectional dimensions of the beam shown in the figure are a = 4.2 in., b = 5.5 in., d = 4.5 in., and t = 0.33 in. The internal bending moment about the z centroidal axis is M, = -4.15 kip-ft. Determine (a) the maximum tension bending stress (a positive number) in the beam. (b) the maximum compression bending stress (a negative number) in the beam. b (typ.) a a Answers: (a) OmaxT psi (b) Omax C = psi

Structural Analysis

6th Edition

ISBN:9781337630931

Author:KASSIMALI, Aslam.

Publisher:KASSIMALI, Aslam.

Chapter2: Loads On Structures

Section: Chapter Questions

Problem 1P

See similar textbooks

Similar questions

Note! [ynore the beam weight Drw the fre boody dayram dugran Hho given benm Fired 2. 6m
2 – (20%) For the beam shown in Figure P-2, draw influence line for reactions at A, B, and shear at C. Also, determine the maximum positive moment that can be developed at point E for a concentrate moving load of 30-kips, a uniform moving load of 0.5 kips/ft, and beam weight of 0.3 kips/ft. A is a pin, B & D are rollers, and C is a hinge.
give illustration or drawing of a model of strong bridge that will use bbq stick and bands.
write and describe the steps and stages of designing a rail of the raiway track
Explain the procedure of the automatic hammer.
Please identify if there are any two-force member.
i need the answer quickly
Brome A-300 mm 120.8m gap-03mm Stel A= 250 tmm L: 12M E<200 Gk E-83 EPA Find for the shess deeloped in each bar.
Where is the point of zero shear?
The width of an outer aircraft panel is uniformly distributed between 1.00 to 1.10 millimeters. Determine the following: a. Proportion of panels that exceed 1.05 millimeters b. Thickness exceeded by 90% of the flanges Choices: a. 0.50. 0.96 b. NONE c. 0.50, 1.01 d. 0.30. 0.96
.In the reinforced beam section shown in the figure (not drawn to scale), the nominal cover provided at the bottom of the beam as per IS 456-2000, is 50 2-286 3-166 x 50 2-legged, 12 strrups@90c/e X 50
4. For the trugs shwn below, identify aäy and all zero førce thembers by placng ak*0" next to or thbugh that member. D