FormulaDen.com

Physics Chemistry Math Chemical Engineering Civil Electrical Electronics Electronics and Instrumentation Materials Science Mechanical Production Engineering Financial Health

Combined Stresses at Topmost Fibre of Cross Section Formula

Fx Copy

LaTeX Copy

Combined Stresses Topmost Fibre Cross Section refers to the combined effect of bending stress and axial stress at the extreme fiber of the cross section. Check FAQs

f 1cs = f cs1 + f 1

f_1cs - Combined Stresses Topmost Fibre Cross Section?f_cs1 - Stress due to Internal Pressure?f₁ - Stress Bending Moment at Topmost of Cross Section?

Combined Stresses at Topmost Fibre of Cross Section Example

With values

With units

Only example

Here is how the Combined Stresses at Topmost Fibre of Cross Section equation looks like with Values.

Here is how the Combined Stresses at Topmost Fibre of Cross Section equation looks like with Units.

Here is how the Combined Stresses at Topmost Fibre of Cross Section equation looks like.

61.197 = 61.19 + 0.007

61.197N/mm² = 61.19N/mm² + 0.007N/mm²

61.197 = 61.19 + 0.007

Tip: Use pencil ( Pencil

) icon above to edit Input Values and Units.

Calculate

Recalculate

Solution

Copy

Reset

You are here -

Home » Category

Engineering » Category

Chemical Engineering » Category

Process Equipment Design » fx Combined Stresses at Topmost Fibre of Cross Section

Combined Stresses at Topmost Fibre of Cross Section Solution

Follow our step by step solution on how to calculate Combined Stresses at Topmost Fibre of Cross Section?

FIRST Step Consider the formula

f 1cs = f cs1 + f 1

Next Step Substitute values of Variables

∴

f 1cs = 61.19N/mm² + 0.007N/mm²

Next Step Convert Units

∴

f 1cs = 6.1E+7Pa + 7000Pa

Next Step Prepare to Evaluate

∴

f 1cs = 6.1E+7 + 7000

Next Step Evaluate

∴

f 1cs = 61197000Pa

LAST Step Convert to Output's Unit

∴

f 1cs = 61.197N/mm²

Combined Stresses at Topmost Fibre of Cross Section Formula Elements

Variables

Combined Stresses Topmost Fibre Cross Section

Combined Stresses Topmost Fibre Cross Section refers to the combined effect of bending stress and axial stress at the extreme fiber of the cross section.

Symbol: f_1cs

Measurement: StressUnit: N/mm²

Note: Value should be greater than 0.

Formulas to find Combined Stresses Topmost Fibre Cross Section

Stress due to Internal Pressure

Stress due to Internal Pressure refers to the amount of pressure-induced stress exerted on the walls of a container or vessel due to the presence of fluids or gases inside.

Symbol: f_cs1

Measurement: StressUnit: N/mm²

Note: Value should be greater than 0.

Formulas to find Stress due to Internal Pressure

Stress Bending Moment at Topmost of Cross Section

The Stress Bending Moment at Topmost of Cross Section refers to the amount of stress that develops at the outermost or topmost layer of a vessel.

Symbol: f₁

Measurement: StressUnit: N/mm²

Note: Value should be greater than 0.

Formulas to find Stress Bending Moment at Topmost of Cross Section

Other formulas in Saddle Support category

Go Combined Stresses at Mid Span

f cs3 = f cs1 + f 3

Go Bending Moment at Support

M 1 = Q \cdot A \cdot ((1) - (\frac{1 - (\frac{A}{L}) + (\frac{{(R vessel)}^{2} - {(Depth Head)}^{2}}{2 \cdot A \cdot L})}{1 + (\frac{4}{3}) \cdot (\frac{Depth Head}{L})}))

Go Combined Stresses at Bottommost Fibre of Cross Section

f cs2 = f cs1 - f 2

Go Corresponding Bending Stress with Section Modulus

f wb = \frac{M w}{Z}

How to Evaluate Combined Stresses at Topmost Fibre of Cross Section?

Combined Stresses at Topmost Fibre of Cross Section evaluator uses Combined Stresses Topmost Fibre Cross Section = Stress due to Internal Pressure+Stress Bending Moment at Topmost of Cross Section to evaluate the Combined Stresses Topmost Fibre Cross Section, Combined Stresses at Topmost Fibre of Cross Section refers to the combined effect of bending stress and axial stress at the extreme fiber of the cross section. Combined Stresses Topmost Fibre Cross Section is denoted by f_1cs symbol.

How to evaluate Combined Stresses at Topmost Fibre of Cross Section using this online evaluator? To use this online evaluator for Combined Stresses at Topmost Fibre of Cross Section, enter Stress due to Internal Pressure (f_cs1) & Stress Bending Moment at Topmost of Cross Section (f₁) and hit the calculate button.

FAQs on Combined Stresses at Topmost Fibre of Cross Section

What is the formula to find Combined Stresses at Topmost Fibre of Cross Section?

The formula of Combined Stresses at Topmost Fibre of Cross Section is expressed as Combined Stresses Topmost Fibre Cross Section = Stress due to Internal Pressure+Stress Bending Moment at Topmost of Cross Section. Here is an example- 6.1E-5 = 61190000+7000.

How to calculate Combined Stresses at Topmost Fibre of Cross Section?

With Stress due to Internal Pressure (f_cs1) & Stress Bending Moment at Topmost of Cross Section (f₁) we can find Combined Stresses at Topmost Fibre of Cross Section using the formula - Combined Stresses Topmost Fibre Cross Section = Stress due to Internal Pressure+Stress Bending Moment at Topmost of Cross Section.

Can the Combined Stresses at Topmost Fibre of Cross Section be negative?

No, the Combined Stresses at Topmost Fibre of Cross Section, measured in Stress cannot be negative.

Which unit is used to measure Combined Stresses at Topmost Fibre of Cross Section?

Combined Stresses at Topmost Fibre of Cross Section is usually measured using the Newton per Square Millimeter[N/mm²] for Stress. Pascal[N/mm²], Newton per Square Meter[N/mm²], Kilonewton per Square Meter[N/mm²] are the few other units in which Combined Stresses at Topmost Fibre of Cross Section can be measured.

Let Others Know

✖

Facebook

Twitter

Copied!

Combined Stresses at Topmost Fibre of Cross Section Formula

Combined Stresses at Topmost Fibre of Cross Section Example

Combined Stresses at Topmost Fibre of Cross Section Solution

Combined Stresses at Topmost Fibre of Cross Section Formula Elements

Other formulas in Saddle Support category

How to Evaluate Combined Stresses at Topmost Fibre of Cross Section?

FAQs on Combined Stresses at Topmost Fibre of Cross Section

Variable Name