508. Determine the minimum width b of the beam shown in Fig. P-508 if the flexural stress is not to exceed 10 MPa. Ans. b- 75.0 mm 5000 N 1 m 2000 N/m 200 mm 1 m 3 m R1 R2 Figure P-508.

Structural Analysis
6th Edition
ISBN:9781337630931
Author:KASSIMALI, Aslam.
Publisher:KASSIMALI, Aslam.
Chapter2: Loads On Structures
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36 ZAIN IQ
bigås - Strength of materials
5-2 Derivation of Flexure Formula
163
507. In a laboratory test of a beam loaded by end couples, the
fibers at layer AB in Fig. P-507 are found to increase 30 x 10-3 mm
while those at CD decrease 90 x 10-3 mm in the 200-mm-gage length.
Using E - 100 GPa, determine the flexural stress in the top and bottom
fibers.
200 mm-
50 mm
A
B
100 mm
D
75 mm
Figure P-507.
508. Determine the minimum width b of the beam shown in Fig.
P-508 if the flexural stress is not to exceed 10 MPa.
Ans. b = 75.0 mm
5000 N
1 m
2000 N/m
200 mm
1 m
3 m
R1
R2
Flgure P-508.
509.
A box section used in aircraft is constructed of tubes
connected by thin webs as shown in Fig. P-509. Each tube has a
cross-sectional area of 130 mm2. If the average stress in the tubes is not
to exceed 70 MPa, determine the total uniformly distributed load that
can be supported on a simple span 4 m long. Neglect the effects of the
webs.
100 mm
100 mm
200 mm
150 mm
Figure P-509.
164
5 Stresses in Beams
510. A 40-mm diameter bar is used as a simply supported beam
2 m long Determine the lareest uniformly distributed load which can be
Transcribed Image Text:36 ZAIN IQ bigås - Strength of materials 5-2 Derivation of Flexure Formula 163 507. In a laboratory test of a beam loaded by end couples, the fibers at layer AB in Fig. P-507 are found to increase 30 x 10-3 mm while those at CD decrease 90 x 10-3 mm in the 200-mm-gage length. Using E - 100 GPa, determine the flexural stress in the top and bottom fibers. 200 mm- 50 mm A B 100 mm D 75 mm Figure P-507. 508. Determine the minimum width b of the beam shown in Fig. P-508 if the flexural stress is not to exceed 10 MPa. Ans. b = 75.0 mm 5000 N 1 m 2000 N/m 200 mm 1 m 3 m R1 R2 Flgure P-508. 509. A box section used in aircraft is constructed of tubes connected by thin webs as shown in Fig. P-509. Each tube has a cross-sectional area of 130 mm2. If the average stress in the tubes is not to exceed 70 MPa, determine the total uniformly distributed load that can be supported on a simple span 4 m long. Neglect the effects of the webs. 100 mm 100 mm 200 mm 150 mm Figure P-509. 164 5 Stresses in Beams 510. A 40-mm diameter bar is used as a simply supported beam 2 m long Determine the lareest uniformly distributed load which can be
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