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Maximum Bending Stress for Load Applied to Narrow Member Face Formula

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Maximum bending stress for load on narrow face is the maximum bending stress (design value) on a section where the load is applied to a narrow face. Check FAQs

F bE = \frac{K cE \cdot E'}{{(R B)}^{2}}

F_bE - Maximum Bending Stress for Load on Narrow Face?K_cE - Euler Buckling Constant?E' - Adjusted Modulus of Elasticity?R_B - Slenderness Ratio?

Maximum Bending Stress for Load Applied to Narrow Member Face Example

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Here is how the Maximum Bending Stress for Load Applied to Narrow Member Face equation looks like with Values.

Here is how the Maximum Bending Stress for Load Applied to Narrow Member Face equation looks like with Units.

Here is how the Maximum Bending Stress for Load Applied to Narrow Member Face equation looks like.

0.125 = \frac{0.7 \cdot 50}{{(16.73)}^{2}}

0.125psi = \frac{0.7 \cdot 50psi}{{(16.73)}^{2}}

0.125 = \frac{0.7 \cdot 50}{{(16.73)}^{2}}

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Maximum Bending Stress for Load Applied to Narrow Member Face Solution

Follow our step by step solution on how to calculate Maximum Bending Stress for Load Applied to Narrow Member Face?

FIRST Step Consider the formula

F bE = \frac{K cE \cdot E'}{{(R B)}^{2}}

Next Step Substitute values of Variables

∴

F bE = \frac{0.7 \cdot 50psi}{{(16.73)}^{2}}

Next Step Prepare to Evaluate

∴

F bE = \frac{0.7 \cdot 50}{{(16.73)}^{2}}

Next Step Evaluate

∴

F bE = 862.174443362626Pa

Next Step Convert to Output's Unit

∴

F bE = 0.125047830795279psi

LAST Step Rounding Answer

∴

F bE = 0.125psi

Maximum Bending Stress for Load Applied to Narrow Member Face Formula Elements

Variables

Maximum Bending Stress for Load on Narrow Face

Maximum bending stress for load on narrow face is the maximum bending stress (design value) on a section where the load is applied to a narrow face.

Symbol: F_bE

Measurement: PressureUnit: psi

Note: Value should be greater than 0.

Formulas to find Maximum Bending Stress for Load on Narrow Face

Euler Buckling Constant

Euler Buckling Constant is a constant for the buckling of column. Here the constant is used for compressive loading.

Symbol: K_cE

Measurement: NAUnit: Unitless

Note: Value should be greater than 0.

Formulas to find Euler Buckling Constant

Adjusted Modulus of Elasticity

Adjusted Modulus of Elasticity is the modulus of elasticity multiplied by adjustment factors in timber design.

Symbol: E'

Measurement: PressureUnit: psi

Note: Value should be greater than 0.

Formulas to find Adjusted Modulus of Elasticity

Slenderness Ratio

Slenderness ratio, or simply slenderness is an aspect ratio, the quotient between the height and the width of a building.

Symbol: R_B

Measurement: NAUnit: Unitless

Note: Value should be greater than 0.

Formulas to find Slenderness Ratio

Other formulas in Bending and Axial Compression category

Go Maximum Compressive Stress for Uniaxial Bending

F cE = (\frac{K cE \cdot E'}{{(\frac{L e1}{d 1})}^{2}})

Go Maximum Compressive Stress for Biaxial Bending

F cE = (\frac{K cE \cdot E'}{{(\frac{L e2}{d 2})}^{2}})

How to Evaluate Maximum Bending Stress for Load Applied to Narrow Member Face?

Maximum Bending Stress for Load Applied to Narrow Member Face evaluator uses Maximum Bending Stress for Load on Narrow Face = (Euler Buckling Constant*Adjusted Modulus of Elasticity)/((Slenderness Ratio)^2) to evaluate the Maximum Bending Stress for Load on Narrow Face, The Maximum Bending Stress for Load Applied to Narrow Member Face formula is defined as the maximum limit of stress that the timber section can survive when the load is applied at the narrow face of section. Maximum Bending Stress for Load on Narrow Face is denoted by F_bE symbol.

How to evaluate Maximum Bending Stress for Load Applied to Narrow Member Face using this online evaluator? To use this online evaluator for Maximum Bending Stress for Load Applied to Narrow Member Face, enter Euler Buckling Constant (K_cE), Adjusted Modulus of Elasticity (E') & Slenderness Ratio (R_B) and hit the calculate button.

FAQs on Maximum Bending Stress for Load Applied to Narrow Member Face

What is the formula to find Maximum Bending Stress for Load Applied to Narrow Member Face?

The formula of Maximum Bending Stress for Load Applied to Narrow Member Face is expressed as Maximum Bending Stress for Load on Narrow Face = (Euler Buckling Constant*Adjusted Modulus of Elasticity)/((Slenderness Ratio)^2). Here is an example- 1.8E-5 = (0.7*344737.864655216)/((16.73)^2).

How to calculate Maximum Bending Stress for Load Applied to Narrow Member Face?

With Euler Buckling Constant (K_cE), Adjusted Modulus of Elasticity (E') & Slenderness Ratio (R_B) we can find Maximum Bending Stress for Load Applied to Narrow Member Face using the formula - Maximum Bending Stress for Load on Narrow Face = (Euler Buckling Constant*Adjusted Modulus of Elasticity)/((Slenderness Ratio)^2).

Can the Maximum Bending Stress for Load Applied to Narrow Member Face be negative?

No, the Maximum Bending Stress for Load Applied to Narrow Member Face, measured in Pressure cannot be negative.

Which unit is used to measure Maximum Bending Stress for Load Applied to Narrow Member Face?

Maximum Bending Stress for Load Applied to Narrow Member Face is usually measured using the Pound Per Square Inch[psi] for Pressure. Pascal[psi], Kilopascal[psi], Bar[psi] are the few other units in which Maximum Bending Stress for Load Applied to Narrow Member Face can be measured.

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Maximum Bending Stress for Load Applied to Narrow Member Face Formula

Maximum Bending Stress for Load Applied to Narrow Member Face Example

Maximum Bending Stress for Load Applied to Narrow Member Face Solution

Maximum Bending Stress for Load Applied to Narrow Member Face Formula Elements

Other formulas in Bending and Axial Compression category

How to Evaluate Maximum Bending Stress for Load Applied to Narrow Member Face?

FAQs on Maximum Bending Stress for Load Applied to Narrow Member Face

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