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

Maximum Bending Moment when Maximum Stress For Short Beams is Given
Maximum Bending Moment=((Maximum stress at crack tip-(Axial Load/Cross sectional area))*Moment of Inertia)/Distance from the Neutral axis GO
Cross-Sectional Area when Maximum Stress For Short Beams is Given
Cross sectional area=Axial Load/(Maximum stress at crack tip-(Maximum Bending Moment*Distance from the Neutral axis/Moment of Inertia)) GO
Axial Load when Maximum Stress For Short Beams is Given
Axial Load=Cross sectional area*(Maximum stress at crack tip-(Maximum Bending Moment*Distance from the Neutral axis/Moment of Inertia)) 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
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
Stress Amplitude
Stress amplitude=(Maximum stress at crack tip-Minimum Stress)/2 GO

3 Other formulas that calculate the same Output

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
Dead load moment when maximum stress in the bottom flange is given
Dead Load Moment= (Maximum stress at crack tip*Section Modulus of Transformed Composite Section)-Live Load Moment 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

Dead load moment when maximum unit stress in steel is given Formula

Dead Load Moment= (Maximum stress at crack tip-(Live Load Moment/ Section Modulus of Transformed Composite Section))*Section Modulus of Steel Beam
M<sub>D</sub>= (σ<sub>m</sub>-(M<sub>L</sub>/ S<sub>tr</sub>))*S<sub>s</sub>
More formulas
Allowable stress in the flanges GO
Yield strength when allowable stress in the flange is given GO
Maximum unit stress in the steel 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 maximum stress?

the maximum stress that the specimen can withstand is called the maximum strength of that particular material.

How to Calculate Dead load moment when maximum unit stress in steel is given?

Dead load moment when maximum unit stress in steel is given calculator uses Dead Load Moment= (Maximum stress at crack tip-(Live Load Moment/ Section Modulus of Transformed Composite Section))*Section Modulus of Steel Beam to calculate the Dead Load Moment, The Dead load moment when maximum unit stress in steel is given can be defined as self weight of the structural member. Dead Load Moment and is denoted by MD symbol.

How to calculate Dead load moment when maximum unit stress in steel is given using this online calculator? To use this online calculator for Dead load moment when maximum unit stress in steel is given, enter Maximum stress at crack tip m), Live Load Moment (ML), Section Modulus of Transformed Composite Section (Str) and Section Modulus of Steel Beam (Ss) and hit the calculate button. Here is how the Dead load moment when maximum unit stress in steel is given calculation can be explained with given input values -> -9.4 = (60000000-(10/ 1E-08))*1E-08.

FAQ

What is Dead load moment when maximum unit stress in steel is given?
The Dead load moment when maximum unit stress in steel is given can be defined as self weight of the structural member and is represented as MD= (σm-(ML/ Str))*Ss or Dead Load Moment= (Maximum stress at crack tip-(Live Load Moment/ Section Modulus of Transformed Composite Section))*Section Modulus of Steel Beam. Maximum stress at crack tip due to the applied nominal stress, Live Load Moment is the moment generated due to dead load acting to member, Section Modulus of Transformed Composite Section, is a geometric property 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 Dead load moment when maximum unit stress in steel is given?
The Dead load moment when maximum unit stress in steel is given can be defined as self weight of the structural member is calculated using Dead Load Moment= (Maximum stress at crack tip-(Live Load Moment/ Section Modulus of Transformed Composite Section))*Section Modulus of Steel Beam. To calculate Dead load moment when maximum unit stress in steel is given, you need Maximum stress at crack tip m), Live Load Moment (ML), Section Modulus of Transformed Composite Section (Str) and Section Modulus of Steel Beam (Ss). With our tool, you need to enter the respective value for Maximum stress at crack tip, Live Load Moment, Section Modulus of Transformed Composite Section 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 Dead Load Moment?
In this formula, Dead Load Moment uses Maximum stress at crack tip, Live Load Moment, Section Modulus of Transformed Composite Section and Section Modulus of Steel Beam. We can use 3 other way(s) to calculate the same, which is/are as follows -
  • Dead Load Moment=Section Modulus of Transformed Composite Section*steel stress-Live Load Moment
  • Dead Load Moment=Section Modulus of Steel Beam*(steel stress-Live Load Moment/Section Modulus of Transformed Composite Section)
  • Dead Load Moment= (Maximum stress at crack tip*Section Modulus of Transformed Composite Section)-Live Load Moment
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