M Naveen
National Institute of Technology (NIT), Warangal
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Mridul Sharma
Indian Institute of Information Technology (IIIT), Bhopal
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11 Other formulas that you can solve using the same Inputs

Dead load moment when maximum unit stress in steel is given
Dead Load Moment= (Maximum stress at crack tip-(Live Load Moment/ Section Modulus of Transformed Composite Section))*Section Modulus of Steel Beam GO
Live load moment when maximum unit stress in steel is given
Live Load Moment= (Maximum stress at crack tip-(Dead Load Moment/Section Modulus of Steel Beam)) *Section Modulus of Transformed Composite Section GO
Section modulus of transformed Composite Section when Stress in Steel for Unshored Members is Given
Section Modulus of Transformed Composite Section=Live Load Moment/(steel stress-(Dead Load Moment/Section Modulus of Steel Beam)) 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
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
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

5 Other formulas that calculate the same Output

Maximum Stress For a Circular Section Under Compression
Maximum stress at crack tip=(0.372+0.056*(Distance from nearest Edge/Radius of gyration)*(Concentrated load/Distance from nearest Edge)*sqrt(Radius of gyration*Distance from nearest Edge)) GO
Maximum Stress For Short Beams
Maximum stress at crack tip=(Axial Load/Cross sectional area)+((Maximum Bending Moment*Distance from the Neutral axis)/Moment of Inertia) GO
The maximum stress in the bottom flange
Maximum stress at crack tip= (Dead Load Moment+Live Load Moment)/ Section Modulus of Transformed Composite Section GO
Maximum Stress For a Rectangular Section Under Compression
Maximum stress at crack tip=(2/3)*Concentrated load/(Height of cross section*Distance from nearest Edge) GO
Maximum stress at crack tip
Maximum stress at crack tip=Stress concentration factor*Applied stress GO

Maximum unit stress in the steel Formula

Maximum stress at crack tip= (Dead Load Moment/Section Modulus of Steel Beam)+(Live Load Moment/Section Modulus of Transformed Composite Section)
σ<sub>m</sub>= (M<sub>D</sub>/S<sub>s</sub>)+(M<sub>L</sub>/S<sub>tr</sub>)
More formulas
Allowable stress in the flanges GO
Yield strength when allowable stress in the flange is given GO
Dead load moment when maximum unit stress in steel is given GO
Live load moment when maximum unit stress in steel is given GO
section modulus of steel beam when maximum unit stress in steel is given GO
Section modulus of transformed composite section when maximum unit stress in steel is given GO
The maximum stress in the bottom flange GO
Dead load moment when maximum stress in the bottom flange is given GO
Live load moment when maximum stress in the bottom flange is given GO
Section modulus of transformed composite section when maximum stress in the bottom flange is given GO

What is live and dead loads?

:-Dead load is defined as eself weight of the structural member whereas :-Live load is defined as weight of movable objects in the structural member.

How to Calculate Maximum unit stress in the steel?

Maximum unit stress in the steel calculator uses Maximum stress at crack tip= (Dead Load Moment/Section Modulus of Steel Beam)+(Live Load Moment/Section Modulus of Transformed Composite Section) to calculate the Maximum stress at crack tip, The Maximum unit stress in the steel can be defined as the maximum stress that the specimen can withstand is called the maximum strength of that particular material. Maximum stress at crack tip and is denoted by σm symbol.

How to calculate Maximum unit stress in the steel using this online calculator? To use this online calculator for Maximum unit stress in the steel, enter Dead Load Moment (MD), Section Modulus of Steel Beam (Ss), Live Load Moment (ML) and Section Modulus of Transformed Composite Section (Str) and hit the calculate button. Here is how the Maximum unit stress in the steel calculation can be explained with given input values -> 2000 = (10/1E-08)+(10/1E-08).

FAQ

What is Maximum unit stress in the steel?
The Maximum unit stress in the steel can be defined as the maximum stress that the specimen can withstand is called the maximum strength of that particular material and is represented as σm= (MD/Ss)+(ML/Str) or Maximum stress at crack tip= (Dead Load Moment/Section Modulus of Steel Beam)+(Live Load Moment/Section Modulus of Transformed Composite Section). Dead Load Moment is the moment generated due to dead load acting to member, Section Modulus of Steel Beam is a geometric property for a given cross-section used in the design of steel beams or flexural members, Live Load Moment is the moment generated due to dead load acting to member and Section Modulus of Transformed Composite Section, is a geometric property.
How to calculate Maximum unit stress in the steel?
The Maximum unit stress in the steel can be defined as the maximum stress that the specimen can withstand is called the maximum strength of that particular material is calculated using Maximum stress at crack tip= (Dead Load Moment/Section Modulus of Steel Beam)+(Live Load Moment/Section Modulus of Transformed Composite Section). To calculate Maximum unit stress in the steel, you need Dead Load Moment (MD), Section Modulus of Steel Beam (Ss), Live Load Moment (ML) and Section Modulus of Transformed Composite Section (Str). With our tool, you need to enter the respective value for Dead Load Moment, Section Modulus of Steel Beam, Live Load Moment and Section Modulus of Transformed Composite Section 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 Maximum stress at crack tip?
In this formula, Maximum stress at crack tip uses Dead Load Moment, Section Modulus of Steel Beam, Live Load Moment and Section Modulus of Transformed Composite Section. We can use 5 other way(s) to calculate the same, which is/are as follows -
  • Maximum stress at crack tip=Stress concentration factor*Applied stress
  • Maximum stress at crack tip=(Axial Load/Cross sectional area)+((Maximum Bending Moment*Distance from the Neutral axis)/Moment of Inertia)
  • Maximum stress at crack tip=(0.372+0.056*(Distance from nearest Edge/Radius of gyration)*(Concentrated load/Distance from nearest Edge)*sqrt(Radius of gyration*Distance from nearest Edge))
  • Maximum stress at crack tip=(2/3)*Concentrated load/(Height of cross section*Distance from nearest Edge)
  • Maximum stress at crack tip= (Dead Load Moment+Live Load Moment)/ Section Modulus of Transformed Composite Section
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