ASTUATION 11.5mB7 kN/m3mCDetermine the FF.• FLEXURAL RIGIDITY, x10¹0 Nmm²• Ocin rad• &c, mm• SA, mm• SE, mm•3 kN/m5mD173 kNwww1.5mEE = 187.5 GPalī 1600X106 mmªuse VWMEQUIVALENT SIMPLY SUPPORTED SPAN IF 8℃ IS CONSERVEDkNAS MAX DEFLECTION. USE w = 15-m

Note: As per bartleby guidelines, only 1st 3 parts among multiple parts need to be solved. For rest…

A STUATION 1 1.5m B 7 kN/m 3m C 3 kN/m 5m D 173 kN www m 1.5m E E = 187.5 GPa lī 1600X106 mmª use VWM Determine the FF. • FLEXURAL RIGIDITY, x10¹0 Nmm² • Ocin rad • &c, mm • SA, mm • SE, mm • EQUIVALENT SIMPLY SUPPORTED SPAN IF 8℃ IS CONSERVED kN AS MAX DEFLECTION. USE @ = 15

A STUATION 1 1.5m B 7 kN/m 3m C 3 kN/m 5m D 173 kN www m 1.5m E E = 187.5 GPa lī 1600X106 mmª use VWM Determine the FF. • FLEXURAL RIGIDITY, x10¹0 Nmm² • Ocin rad • &c, mm • SA, mm • SE, mm • EQUIVALENT SIMPLY SUPPORTED SPAN IF 8℃ IS CONSERVED kN AS MAX DEFLECTION. USE @ = 15

Structural Analysis

6th Edition

ISBN:9781337630931

Author:KASSIMALI, Aslam.

Publisher:KASSIMALI, Aslam.

Chapter2: Loads On Structures

Section: Chapter Questions

Problem 1P

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Question

A
STUATION 1
1.5m
B
7 kN/m
3m
C
Determine the FF.
• FLEXURAL RIGIDITY, x10¹0 Nmm²
• Ocin rad
• &c, mm
• SA, mm
• SE, mm
•
3 kN/m
5m
D
173 kN
www
1.5m
E
E = 187.5 GPa
lī 1600X106 mmª
use VWM
EQUIVALENT SIMPLY SUPPORTED SPAN IF 8℃ IS CONSERVED
kN
AS MAX DEFLECTION. USE w = 15-
m

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