Live load moment when maximum stress in the bottom flange is given Calculator

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✖Maximum stress at crack tip due to the applied nominal stress.ⓘ Maximum stress at crack tip [σ_m]			+10% -10%
✖Section Modulus of Transformed Composite Section, is a geometric property.ⓘ Section Modulus of Transformed Composite Section [S_tr]			+10% -10%
✖Dead Load Moment is the moment generated due to dead load acting to member.ⓘ Dead Load Moment [M_D]			+10% -10%

✖Live Load Moment is the moment generated due to dead load acting to member.ⓘ Live load moment when maximum stress in the bottom flange is given [M_L]

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Live load moment when maximum stress in the bottom flange is given

M Naveen

National Institute of Technology (NIT), Warangal

M Naveen has created this Calculator and 100+ more calculators!

Mridul Sharma

Indian Institute of Information Technology (IIIT), Bhopal

Mridul Sharma has verified this Calculator and 200+ more calculators!

< 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

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

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

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

Live load moment when maximum stress in the bottom flange is given Formula

Live Load Moment= (Maximum stress at crack tip*Section Modulus of Transformed Composite Section)-Dead Load Moment
ML= (σm*Str)-MD

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

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

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 Live load moment when maximum stress in the bottom flange is given?

Live load moment when maximum stress in the bottom flange is given calculator uses Live Load Moment= (Maximum stress at crack tip*Section Modulus of Transformed Composite Section)-Dead Load Moment to calculate the Live Load Moment, The Live load moment when maximum stress in the bottom flange is given can be defined as the weight of movable objects in the structural member. Live Load Moment and is denoted by M_L symbol.

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

FAQ

What is Live load moment when maximum stress in the bottom flange is given?

The Live load moment when maximum stress in the bottom flange is given can be defined as the weight of movable objects in the structural member and is represented as M_L= (σ_m*S_tr)-M_D or Live Load Moment= (Maximum stress at crack tip*Section Modulus of Transformed Composite Section)-Dead Load Moment. Maximum stress at crack tip due to the applied nominal stress, Section Modulus of Transformed Composite Section, is a geometric property and Dead Load Moment is the moment generated due to dead load acting to member.

How to calculate Live load moment when maximum stress in the bottom flange is given?

The Live load moment when maximum stress in the bottom flange is given can be defined as the weight of movable objects in the structural member is calculated using Live Load Moment= (Maximum stress at crack tip*Section Modulus of Transformed Composite Section)-Dead Load Moment. To calculate Live load moment when maximum stress in the bottom flange is given, you need Maximum stress at crack tip (σ_m), Section Modulus of Transformed Composite Section (S_tr) and Dead Load Moment (M_D). With our tool, you need to enter the respective value for Maximum stress at crack tip, Section Modulus of Transformed Composite Section and Dead Load Moment 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 Live Load Moment?

In this formula, Live Load Moment uses Maximum stress at crack tip, Section Modulus of Transformed Composite Section and Dead Load Moment. We can use 3 other way(s) to calculate the same, which is/are as follows -

Live Load Moment=Section Modulus of Transformed Composite Section*steel stress-Dead Load Moment
Live Load Moment=Section Modulus of Transformed Composite Section*(steel stress-Dead Load Moment/Section Modulus of Steel Beam)
Live Load Moment= (Maximum stress at crack tip-(Dead Load Moment/Section Modulus of Steel Beam)) *Section Modulus of Transformed Composite Section

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