Rithik Agrawal
National Institute of Technology Karnataka (NITK), Surathkal
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Chandana P Dev
NSS College of Engineering (NSSCE), Palakkad
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11 Other formulas that you can solve using the same Inputs

Stress in Compressive Steel
stress in compressive steel=(Distance from compression fiber to NA-Effective cover/(Centroidal distance of tension reinforcement-Distance from compression fiber to NA))*(2*steel stress) GO
Section Modulus of Steel Beam when Stress in Steel for Unshored Members is Given
Section Modulus of Steel Beam=Dead Load Moment/(steel stress-(Live Load Moment/Section Modulus of Transformed Composite Section)) GO
Stress in Steel for Unshored Members
steel stress=(Dead Load Moment/Section Modulus of Steel Beam)+(Live Load Moment/Section Modulus of Transformed Composite Section) GO
Live Load Moment when Stress in Steel for Unshored Members is Given
Live Load Moment=Section Modulus of Transformed Composite Section*(steel stress-Dead Load Moment/Section Modulus of Steel Beam) GO
Dead Load Moment when Stress in Steel for Unshored Members is Given
Dead Load Moment=Section Modulus of Steel Beam*(steel stress-Live Load Moment/Section Modulus of Transformed Composite Section) GO
Moment Resistance of Tensile Steel when Area is Given
Moment resistance of tensile steel=(Area of steel required)*(steel stress)*(Distance between reinforcements) GO
Stress in Steel for Shored Members
steel stress=(Dead Load Moment+Live Load Moment)/Section Modulus of Transformed Composite Section GO
Dead Load Moment when Stress in Steel for Shored Members is Given
Dead Load Moment=Section Modulus of Transformed Composite Section*steel stress-Live Load Moment GO
Live Load Moment when Stress in Steel for Shored Members is Given
Live Load Moment=Section Modulus of Transformed Composite Section*steel stress-Dead Load Moment GO
Distance from Extreme Compression Surface to Neutral Axis in Compression Failure
Neutral axis depth=(0.003*Effective depth)/((steel stress/modulus of elasticity)+0.003) GO
Equation Based on Linear Variation of Stress and Strain with Distance
Ratio of depth=1/(1+(steel stress/(Modular Ratio*Compressive stress of concrete))) GO

3 Other formulas that calculate the same Output

Section modulus of transformed composite section when maximum unit stress in steel is given
Section Modulus of Transformed Composite Section= Live Load Moment/(Maximum stress at crack tip-(Dead Load Moment/Section Modulus of Steel Beam)) GO
Section modulus of transformed composite section when maximum stress in the bottom flange is given
Section Modulus of Transformed Composite Section= (Dead Load Moment+Live Load Moment)/Maximum stress at crack tip GO
Section modulus of transformed Composite Section when Stress in Steel for shored Members is Given
Section Modulus of Transformed Composite Section=(Dead Load Moment+Live Load Moment)/steel stress GO

Section modulus of transformed Composite Section when Stress in Steel for Unshored Members is Given Formula

Section Modulus of Transformed Composite Section=Live Load Moment/(steel stress-(Dead Load Moment/Section Modulus of Steel Beam))
S<sub>tr</sub>=M<sub>L</sub>/(f<sub>s</sub>-(M<sub>D</sub>/S<sub>s</sub>))
More formulas
Stress in Steel for Unshored Members GO
Stress in Steel for Shored Members GO
Dead Load Moment when Stress in Steel for Shored Members is Given GO
Live Load Moment when Stress in Steel for Shored Members is Given GO
Live Load Moment when Stress in Steel for Unshored Members is Given GO
Dead Load Moment when Stress in Steel for Unshored Members is Given GO
Section Modulus of Steel Beam when Stress in Steel for Unshored Members is Given GO
Section modulus of transformed Composite Section when Stress in Steel for shored Members is Given GO

What is Section Modulus of Transformed Section ?

Section Modulus of Transformed Section if defined when we use the theory of the transformed-section method is well known and generally accepted as a method of analysis of members loaded in bending. of a composite member, distorted based upon the relative strength of the materials comprising the member, which in turn is used for the analysis of that member, for finding section modulus.

How to Calculate Section modulus of transformed Composite Section when Stress in Steel for Unshored Members is Given?

Section modulus of transformed Composite Section when Stress in Steel for Unshored Members is Given calculator uses Section Modulus of Transformed Composite Section=Live Load Moment/(steel stress-(Dead Load Moment/Section Modulus of Steel Beam)) to calculate the Section Modulus of Transformed Composite Section, The Section modulus of transformed Composite Section when Stress in Steel for Unshored Members is Given formula is defined as the ratio of moment of inertia to distance of extreme fiber for composite section. Section Modulus of Transformed Composite Section and is denoted by Str symbol.

How to calculate Section modulus of transformed Composite Section when Stress in Steel for Unshored Members is Given using this online calculator? To use this online calculator for Section modulus of transformed Composite Section when Stress in Steel for Unshored Members is Given, enter Live Load Moment (ML), steel stress (fs), Dead Load Moment (MD) and Section Modulus of Steel Beam (Ss) and hit the calculate button. Here is how the Section modulus of transformed Composite Section when Stress in Steel for Unshored Members is Given calculation can be explained with given input values -> -32.203602 = 10/(689475729.310432-(10/1E-08)).

FAQ

What is Section modulus of transformed Composite Section when Stress in Steel for Unshored Members is Given?
The Section modulus of transformed Composite Section when Stress in Steel for Unshored Members is Given formula is defined as the ratio of moment of inertia to distance of extreme fiber for composite section and is represented as Str=ML/(fs-(MD/Ss)) or Section Modulus of Transformed Composite Section=Live Load Moment/(steel stress-(Dead Load Moment/Section Modulus of Steel Beam)). Live Load Moment is the moment generated due to dead load acting to member, steel stress is the stress developed in steel, Dead Load Moment is the moment generated due to dead load acting to member and Section Modulus of Steel Beam is a geometric property for a given cross-section used in the design of steel beams or flexural members.
How to calculate Section modulus of transformed Composite Section when Stress in Steel for Unshored Members is Given?
The Section modulus of transformed Composite Section when Stress in Steel for Unshored Members is Given formula is defined as the ratio of moment of inertia to distance of extreme fiber for composite section is calculated using Section Modulus of Transformed Composite Section=Live Load Moment/(steel stress-(Dead Load Moment/Section Modulus of Steel Beam)). To calculate Section modulus of transformed Composite Section when Stress in Steel for Unshored Members is Given, you need Live Load Moment (ML), steel stress (fs), Dead Load Moment (MD) and Section Modulus of Steel Beam (Ss). With our tool, you need to enter the respective value for Live Load Moment, steel stress, Dead Load Moment and Section Modulus of Steel Beam and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.
How many ways are there to calculate Section Modulus of Transformed Composite Section?
In this formula, Section Modulus of Transformed Composite Section uses Live Load Moment, steel stress, Dead Load Moment and Section Modulus of Steel Beam. We can use 3 other way(s) to calculate the same, which is/are as follows -
  • Section Modulus of Transformed Composite Section=(Dead Load Moment+Live Load Moment)/steel stress
  • Section Modulus of Transformed Composite Section= Live Load Moment/(Maximum stress at crack tip-(Dead Load Moment/Section Modulus of Steel Beam))
  • Section Modulus of Transformed Composite Section= (Dead Load Moment+Live Load Moment)/Maximum stress at crack tip
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