Specified Minimum Yield Stress for Web given Limiting Laterally Unbraced Length Solution

STEP 0: Pre-Calculation Summary
Formula Used
Specified Minimum Yield Stress = ((Radius of Gyration about Minor Axis*Beam Buckling Factor 1*sqrt(1+sqrt(1+(Beam Buckling Factor 2*Smaller Yield Stress^2))))/Limiting Length)+Compressive Residual Stress in Flange
Fyw = ((ry*X1*sqrt(1+sqrt(1+(X2*Fl^2))))/Llim)+Fr
This formula uses 1 Functions, 7 Variables
Functions Used
sqrt - A square root function is a function that takes a non-negative number as an input and returns the square root of the given input number., sqrt(Number)
Variables Used
Specified Minimum Yield Stress - (Measured in Megapascal) - Specified Minimum Yield Stress represents the minimum tensile stress or yield stress required by the flexural member, ex- web.
Radius of Gyration about Minor Axis - (Measured in Meter) - Radius of Gyration about Minor Axis is the root mean square distance of the object's parts from either its center of mass or a given minor axis, depending on the relevant application.
Beam Buckling Factor 1 - Beam Buckling Factor 1 is the value which is considered as the factor of safety against buckling to currently applied loads.
Beam Buckling Factor 2 - Beam Buckling Factor 2 is the value used as factor of safety against buckling by applied loads.
Smaller Yield Stress - (Measured in Megapascal) - Smaller Yield Stress is the yield stress value, which is smallest among, yield stress in web, flange or residual stress.
Limiting Length - (Measured in Meter) - Limiting Length is the maximum length of a structural member before certain design considerations, such as buckling, vibration, and deflection, become critical.
Compressive Residual Stress in Flange - (Measured in Megapascal) - Compressive Residual Stress in Flange is the stress formed after plastic deformation, if the residue at a location has a value of -100 MPa, it is said to be compressive residual stress.
STEP 1: Convert Input(s) to Base Unit
Radius of Gyration about Minor Axis: 20 Millimeter --> 0.02 Meter (Check conversion ​here)
Beam Buckling Factor 1: 3005 --> No Conversion Required
Beam Buckling Factor 2: 64 --> No Conversion Required
Smaller Yield Stress: 110 Megapascal --> 110 Megapascal No Conversion Required
Limiting Length: 30235 Millimeter --> 30.235 Meter (Check conversion ​here)
Compressive Residual Stress in Flange: 80 Megapascal --> 80 Megapascal No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
Fyw = ((ry*X1*sqrt(1+sqrt(1+(X2*Fl^2))))/Llim)+Fr --> ((0.02*3005*sqrt(1+sqrt(1+(64*110^2))))/30.235)+80
Evaluating ... ...
Fyw = 139.000079021248
STEP 3: Convert Result to Output's Unit
139000079.021248 Pascal -->139.000079021248 Megapascal (Check conversion ​here)
FINAL ANSWER
139.000079021248 139.0001 Megapascal <-- Specified Minimum Yield Stress
(Calculation completed in 00.039 seconds)

Credits

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Created by Chandana P Dev
NSS College of Engineering (NSSCE), Palakkad
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Verified by Ishita Goyal
Meerut Institute of Engineering and Technology (MIET), Meerut
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Beams Calculators

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Maximum Laterally Unbraced Length for Plastic Analysis in Solid Bars and Box Beams
​ LaTeX ​ Go Laterally Unbraced Length for Plastic Analysis = (Radius of Gyration about Minor Axis*(5000+3000*(Smaller Moments of Unbraced Beam/Plastic Moment)))/Yield Stress of Steel
Limiting Laterally Unbraced Length for Full Plastic Bending Capacity for I and Channel Sections
​ LaTeX ​ Go Limiting Laterally Unbraced Length = (300*Radius of Gyration about Minor Axis)/sqrt(Flange Yield Stress)
Plastic Moment
​ LaTeX ​ Go Plastic Moment = Specified Minimum Yield Stress*Plastic Modulus

Specified Minimum Yield Stress for Web given Limiting Laterally Unbraced Length Formula

​LaTeX ​Go
Specified Minimum Yield Stress = ((Radius of Gyration about Minor Axis*Beam Buckling Factor 1*sqrt(1+sqrt(1+(Beam Buckling Factor 2*Smaller Yield Stress^2))))/Limiting Length)+Compressive Residual Stress in Flange
Fyw = ((ry*X1*sqrt(1+sqrt(1+(X2*Fl^2))))/Llim)+Fr

What is Residual Stress?

The Residual Stresses are those stresses that remain in an object (in particular, in a welded component) even in the absence of external loading or thermal gradients. In some cases, residual stresses result in significant plastic deformation, leading to warping and distortion of an object.

How to Calculate Specified Minimum Yield Stress for Web given Limiting Laterally Unbraced Length?

Specified Minimum Yield Stress for Web given Limiting Laterally Unbraced Length calculator uses Specified Minimum Yield Stress = ((Radius of Gyration about Minor Axis*Beam Buckling Factor 1*sqrt(1+sqrt(1+(Beam Buckling Factor 2*Smaller Yield Stress^2))))/Limiting Length)+Compressive Residual Stress in Flange to calculate the Specified Minimum Yield Stress, The Specified Minimum Yield Stress for Web given Limiting Laterally Unbraced Length formula is defined as the minimum stress on the web section which involves the relationship between various parameters like buckling factors, radius of gyration, limiting unbraced length and web and flange stresses. Specified Minimum Yield Stress is denoted by Fyw symbol.

How to calculate Specified Minimum Yield Stress for Web given Limiting Laterally Unbraced Length using this online calculator? To use this online calculator for Specified Minimum Yield Stress for Web given Limiting Laterally Unbraced Length, enter Radius of Gyration about Minor Axis (ry), Beam Buckling Factor 1 (X1), Beam Buckling Factor 2 (X2), Smaller Yield Stress (Fl), Limiting Length (Llim) & Compressive Residual Stress in Flange (Fr) and hit the calculate button. Here is how the Specified Minimum Yield Stress for Web given Limiting Laterally Unbraced Length calculation can be explained with given input values -> 0.000139 = ((0.02*3005*sqrt(1+sqrt(1+(64*110000000^2))))/30.235)+80000000.

FAQ

What is Specified Minimum Yield Stress for Web given Limiting Laterally Unbraced Length?
The Specified Minimum Yield Stress for Web given Limiting Laterally Unbraced Length formula is defined as the minimum stress on the web section which involves the relationship between various parameters like buckling factors, radius of gyration, limiting unbraced length and web and flange stresses and is represented as Fyw = ((ry*X1*sqrt(1+sqrt(1+(X2*Fl^2))))/Llim)+Fr or Specified Minimum Yield Stress = ((Radius of Gyration about Minor Axis*Beam Buckling Factor 1*sqrt(1+sqrt(1+(Beam Buckling Factor 2*Smaller Yield Stress^2))))/Limiting Length)+Compressive Residual Stress in Flange. Radius of Gyration about Minor Axis is the root mean square distance of the object's parts from either its center of mass or a given minor axis, depending on the relevant application, Beam Buckling Factor 1 is the value which is considered as the factor of safety against buckling to currently applied loads, Beam Buckling Factor 2 is the value used as factor of safety against buckling by applied loads, Smaller Yield Stress is the yield stress value, which is smallest among, yield stress in web, flange or residual stress, Limiting Length is the maximum length of a structural member before certain design considerations, such as buckling, vibration, and deflection, become critical & Compressive Residual Stress in Flange is the stress formed after plastic deformation, if the residue at a location has a value of -100 MPa, it is said to be compressive residual stress.
How to calculate Specified Minimum Yield Stress for Web given Limiting Laterally Unbraced Length?
The Specified Minimum Yield Stress for Web given Limiting Laterally Unbraced Length formula is defined as the minimum stress on the web section which involves the relationship between various parameters like buckling factors, radius of gyration, limiting unbraced length and web and flange stresses is calculated using Specified Minimum Yield Stress = ((Radius of Gyration about Minor Axis*Beam Buckling Factor 1*sqrt(1+sqrt(1+(Beam Buckling Factor 2*Smaller Yield Stress^2))))/Limiting Length)+Compressive Residual Stress in Flange. To calculate Specified Minimum Yield Stress for Web given Limiting Laterally Unbraced Length, you need Radius of Gyration about Minor Axis (ry), Beam Buckling Factor 1 (X1), Beam Buckling Factor 2 (X2), Smaller Yield Stress (Fl), Limiting Length (Llim) & Compressive Residual Stress in Flange (Fr). With our tool, you need to enter the respective value for Radius of Gyration about Minor Axis, Beam Buckling Factor 1, Beam Buckling Factor 2, Smaller Yield Stress, Limiting Length & Compressive Residual Stress in Flange 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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