Chandana P Dev
NSS College of Engineering (NSSCE), Palakkad
Chandana P Dev has created this Calculator and 100+ more calculators!
Ishita Goyal
Meerut Institute of Engineering and Technology (MIET), Meerut
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11 Other formulas that you can solve using the same Inputs

Deflection for Hollow Rectangle When Load in Middle
Deflection of Beam=(Greatest Safe Load*Length of the Beam^3)/(32*(Sectional Area*(Depth of the Beam^2)-Interior Cross-Sectional Area of Beam*(Interior Depth of the Beam^2))) GO
Deflection for Hollow Rectangle When Load is Distributed
Deflection of Beam=Greatest Safe Load*(Length of the Beam^3)/(52*(Sectional Area*Depth of the Beam^-Interior Cross-Sectional Area of Beam*Interior Depth of the Beam^2)) GO
Greatest Safe Load for Hollow Rectangle When Load is Distributed
Greatest Safe Load=1780*(Sectional Area*Depth of the Beam-Interior Cross-Sectional Area of Beam*Interior Depth of the Beam)/Distance between Supports GO
Greatest Safe Load for Hollow Rectangle When Load in Middle
Greatest Safe Load=(890*(Sectional Area*Depth of the Beam-Interior Cross-Sectional Area of Beam*Interior Depth of the Beam))/Length of the Beam GO
Deflection for Solid Rectangle When Load is Distributed
Deflection of Beam=(Greatest safe distributed load*Length of the Beam^3)/(52*Sectional Area*Depth of the Beam^2) GO
Deflection for Solid Rectangle When Load in Middle
Deflection of Beam=(Greatest Safe Load*Length of the Beam^3)/(32*Sectional Area*Depth of the Beam^2) GO
Greatest Safe Load for Solid Rectangle When Load is Distributed
Greatest safe distributed load=1780*Sectional Area*Depth of the Beam/Length of the Beam GO
Greatest Safe Load for Solid Cylinder When Load is Distributed
Greatest Safe Load=1333*(Sectional Area*Depth of the Beam)/Length of the Beam GO
Greatest Safe Load for Solid Cylinder When Load in Middle
Greatest Safe Load=(667*Sectional Area*Depth of the Beam)/Length of the Beam GO
Greatest Safe Load for Solid Rectangle When Load in Middle
Greatest Safe Load=890*Sectional Area*Depth of the Beam/Length of the Beam GO
Stress in Concrete
Stress=2*Bending moment/(Ratio k*Ratio j*Beam Width*Depth of the Beam^2) GO

4 Other formulas that calculate the same Output

Allowable Stress when Simplifying Term is Between 0.2 and 1
Maximum fiber stress=((2-Simplifying term for Fb)*minimum specified yield stress of steel)/3 GO
Allowable Stress when Simplifying Term is Greater than 1
Maximum fiber stress=minimum specified yield stress of steel/(3*Simplifying term for Fb) GO
Maximum Fiber Stress in Bending for Laterally Supported Noncompact Beams and Girders
Maximum fiber stress=0.60*minimum specified yield stress of steel GO
Maximum Fiber Stress in Bending for Laterally Supported Compact Beams and Girders
Maximum fiber stress=0.66*minimum specified yield stress of steel GO

Allowable Stress when Area of Compression Flange is Solid and Not Less than Tension Flange Formula

Maximum fiber stress=12000*Moment Gradient Factor/((Unbraced Length of the member*Depth of the Beam)/Area of compression flange)
F<sub>b</sub>=12000*C<sub>b</sub>/((L*D)/A<sub>f</sub>)
More formulas
Maximum Fiber Stress in Bending for Laterally Supported Compact Beams and Girders GO
Maximum Fiber Stress in Bending for Laterally Supported Noncompact Beams and Girders GO
Maximum Unsupported Length of Compression Flange-1 GO
Maximum Unsupported Length of Compression Flange-2 GO
Modifier for Moment Gradient GO
Simplifying Term for Allowable Stress Equations GO
Allowable Stress when Simplifying Term is Between 0.2 and 1 GO
Allowable Stress when Simplifying Term is Greater than 1 GO

What is the use of above equation?

When the allowable stress when area of compression flange is solid and not less than tension flange formula is applied (not for channels), the value should always be greater than 0.60 Fy.

How to Calculate Allowable Stress when Area of Compression Flange is Solid and Not Less than Tension Flange?

Allowable Stress when Area of Compression Flange is Solid and Not Less than Tension Flange calculator uses Maximum fiber stress=12000*Moment Gradient Factor/((Unbraced Length of the member*Depth of the Beam)/Area of compression flange) to calculate the Maximum fiber stress, Allowable Stress when Area of Compression Flange is Solid and Not Less than Tension Flange formula is defined by the parameters, moment gradient factor, unbraced length of beam, beam depth and area of compression flange, and unit ksi. Maximum fiber stress and is denoted by Fb symbol.

How to calculate Allowable Stress when Area of Compression Flange is Solid and Not Less than Tension Flange using this online calculator? To use this online calculator for Allowable Stress when Area of Compression Flange is Solid and Not Less than Tension Flange, enter Moment Gradient Factor (Cb), Unbraced Length of the member (L), Depth of the Beam (D) and Area of compression flange (Af) and hit the calculate button. Here is how the Allowable Stress when Area of Compression Flange is Solid and Not Less than Tension Flange calculation can be explained with given input values -> 0.00221 = 12000*1/((0.1*0.254000000001016)/0.0322580000002581).

FAQ

What is Allowable Stress when Area of Compression Flange is Solid and Not Less than Tension Flange?
Allowable Stress when Area of Compression Flange is Solid and Not Less than Tension Flange formula is defined by the parameters, moment gradient factor, unbraced length of beam, beam depth and area of compression flange, and unit ksi and is represented as Fb=12000*Cb/((L*D)/Af) or Maximum fiber stress=12000*Moment Gradient Factor/((Unbraced Length of the member*Depth of the Beam)/Area of compression flange). Moment Gradient Factor is rate at which moment is changing with length of beam, Unbraced length of the member is defined as the distance between adjacent Points, Depth of the Beam is the overall depth of the cross section of the beam perpendicular to the axis of the beam and Area of compression flange is the product of length and depth of the compression flange of the beam. .
How to calculate Allowable Stress when Area of Compression Flange is Solid and Not Less than Tension Flange?
Allowable Stress when Area of Compression Flange is Solid and Not Less than Tension Flange formula is defined by the parameters, moment gradient factor, unbraced length of beam, beam depth and area of compression flange, and unit ksi is calculated using Maximum fiber stress=12000*Moment Gradient Factor/((Unbraced Length of the member*Depth of the Beam)/Area of compression flange). To calculate Allowable Stress when Area of Compression Flange is Solid and Not Less than Tension Flange, you need Moment Gradient Factor (Cb), Unbraced Length of the member (L), Depth of the Beam (D) and Area of compression flange (Af). With our tool, you need to enter the respective value for Moment Gradient Factor, Unbraced Length of the member, Depth of the Beam and Area of compression flange 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 fiber stress?
In this formula, Maximum fiber stress uses Moment Gradient Factor, Unbraced Length of the member, Depth of the Beam and Area of compression flange. We can use 4 other way(s) to calculate the same, which is/are as follows -
  • Maximum fiber stress=0.66*minimum specified yield stress of steel
  • Maximum fiber stress=0.60*minimum specified yield stress of steel
  • Maximum fiber stress=((2-Simplifying term for Fb)*minimum specified yield stress of steel)/3
  • Maximum fiber stress=minimum specified yield stress of steel/(3*Simplifying term for Fb)
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