Section Modulus of Transformed Composite Section given Maximum Stress in Bottom Flange Solution

STEP 0: Pre-Calculation Summary
Formula Used
Section Modulus of Transformed Section = (Dead Load Moment+Live Load Moment)/Maximum Stress
Str = (MD+ML)/σmax
This formula uses 4 Variables
Variables Used
Section Modulus of Transformed Section - (Measured in Cubic Meter) - Section Modulus of Transformed Section is the MOI of a composite beam transformed into an equivalent cross-section (called the transformed section) of an imaginary beam composed of only one material.
Dead Load Moment - (Measured in Newton Meter) - Dead Load Moment is the moment generated due to dead load acting to member.
Live Load Moment - (Measured in Newton Meter) - Live Load Moment is the moment generated due to live load acting to member.
Maximum Stress - (Measured in Pascal) - Maximum Stress is the stress that material or section withstands before its fracture.
STEP 1: Convert Input(s) to Base Unit
Dead Load Moment: 280 Newton Millimeter --> 0.28 Newton Meter (Check conversion ​here)
Live Load Moment: 115 Newton Millimeter --> 0.115 Newton Meter (Check conversion ​here)
Maximum Stress: 2.18 Newton per Square Millimeter --> 2180000 Pascal (Check conversion ​here)
STEP 2: Evaluate Formula
Substituting Input Values in Formula
Str = (MD+ML)/σmax --> (0.28+0.115)/2180000
Evaluating ... ...
Str = 1.81192660550459E-07
STEP 3: Convert Result to Output's Unit
1.81192660550459E-07 Cubic Meter -->181.192660550459 Cubic Millimeter (Check conversion ​here)
FINAL ANSWER
181.192660550459 181.1927 Cubic Millimeter <-- Section Modulus of Transformed Section
(Calculation completed in 00.020 seconds)

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Section Modulus of Transformed Composite Section given Maximum Stress in Bottom Flange Formula

​LaTeX ​Go
Section Modulus of Transformed Section = (Dead Load Moment+Live Load Moment)/Maximum Stress
Str = (MD+ML)/σmax

What is Maximum Stress?

The Maximum Stress can be defined as the maximum stress that the specimen can withstand is called the maximum strength of that particular material.

What is Live and Dead Loads?

The Dead Load is defined as the self-weight of the structural member whereas Live Load is defined as the weight of movable objects in the structural member.

How to Calculate Section Modulus of Transformed Composite Section given Maximum Stress in Bottom Flange?

Section Modulus of Transformed Composite Section given Maximum Stress in Bottom Flange calculator uses Section Modulus of Transformed Section = (Dead Load Moment+Live Load Moment)/Maximum Stress to calculate the Section Modulus of Transformed Section, The Section modulus of transformed composite section given maximum stress in bottom flange can be defined as a geometric property for a given cross-section used in the design of beams or flexural members. Section Modulus of Transformed Section is denoted by Str symbol.

How to calculate Section Modulus of Transformed Composite Section given Maximum Stress in Bottom Flange using this online calculator? To use this online calculator for Section Modulus of Transformed Composite Section given Maximum Stress in Bottom Flange, enter Dead Load Moment (MD), Live Load Moment (ML) & Maximum Stress max) and hit the calculate button. Here is how the Section Modulus of Transformed Composite Section given Maximum Stress in Bottom Flange calculation can be explained with given input values -> 1.7E+11 = (0.28+0.115)/2180000.

FAQ

What is Section Modulus of Transformed Composite Section given Maximum Stress in Bottom Flange?
The Section modulus of transformed composite section given maximum stress in bottom flange can be defined as a geometric property for a given cross-section used in the design of beams or flexural members and is represented as Str = (MD+ML)/σmax or Section Modulus of Transformed Section = (Dead Load Moment+Live Load Moment)/Maximum Stress. Dead Load Moment is the moment generated due to dead load acting to member, Live Load Moment is the moment generated due to live load acting to member & Maximum Stress is the stress that material or section withstands before its fracture.
How to calculate Section Modulus of Transformed Composite Section given Maximum Stress in Bottom Flange?
The Section modulus of transformed composite section given maximum stress in bottom flange can be defined as a geometric property for a given cross-section used in the design of beams or flexural members is calculated using Section Modulus of Transformed Section = (Dead Load Moment+Live Load Moment)/Maximum Stress. To calculate Section Modulus of Transformed Composite Section given Maximum Stress in Bottom Flange, you need Dead Load Moment (MD), Live Load Moment (ML) & Maximum Stress max). With our tool, you need to enter the respective value for Dead Load Moment, Live Load Moment & Maximum Stress and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.
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