Maximum Stress For a Circular Section Under Compression Calculator

Category	Engineering ↺
Engineering	Civil ↺
Civil	Columns ↺
Columns	Eccentric Loads on Columns ↺

✖Distance from nearest Edge is the distance beatween the closest edge of sections and a point load acting on same section.ⓘ Distance from nearest Edge [k]			+10% -10%
✖Radius of gyration or gyradius of a body about an axis of rotation is defined as the radial distance to a point which would have a moment of inertia the same as the body's actual distribution of mass, if the total mass of the body were concentrated there.ⓘ Radius of gyration [k_G]			+10% -10%
✖Concentrated load is a load acting at a single point.ⓘ Concentrated load [P]			+10% -10%

✖Maximum stress at crack tip due to the applied nominal stress.ⓘ Maximum Stress For a Circular Section Under Compression [σ_m]

⎘ Copy

👎 Report Issue!

👍 Share Now!

You are here:

Home »
Engineering »
Civil »
Columns »
Eccentric Loads on Columns »
Maximum Stress For a Circular Section Under Compression

Rudrani Tidke

Cummins College of Engineering for Women (CCEW), Pune

Rudrani Tidke has created this Calculator and 100+ more calculators!

Alithea Fernandes

Don Bosco College of Engineering (DBCE), Goa

Alithea Fernandes has verified this Calculator and 100+ more calculators!

< 11 Other formulas that you can solve using the same Inputs

Periodic time of SHM for compound pendulum in terms of radius of gyration

Periodic time for compound pendulum=2*pi*sqrt(((Radius of gyration^2)+(Distance of point of suspension of pendulum from the center of gravity^2))/(Acceleration Due To Gravity*Distance of point of suspension of pendulum from the center of gravity)) GO

Theoretical Maximum Stress for Secant Code Steels

Critical stress=Yield Strength/(1+((Eccentricity*End Fixity Coefficient/(Radius of gyration^2))*(sec((1/Radius of gyration)*sqrt(Concentrated load/(4*Cross sectional area*Modulus Of Elasticity)))))) GO

Theoretical Maximum Stress for Johnson Code Steels

Critical stress=Yield Strength*(1-(Stress at any point y/(4*Coefficient for Column End Conditions*(pi^2)*Modulus Of Elasticity))*((Length/Radius of gyration)^2)) GO

Euler's Formula for Critical Buckling Load when Area is Given

Critical Buckling Load=(Coefficient for Column End Conditions*(pi^2)*Modulus Of Elasticity*Cross sectional area)/((Length/Radius of gyration)^2) GO

Total Unit Stress in Eccentric Loading when Radius of Gyration is Given

Total Unit Stress=(Axial Load/Cross sectional area)*(1+(Outermost Fiber Distance*Distance_from Load Applied/(Radius of gyration^2))) GO

Time period of Rolling

Time period of rolling=2*pi*(sqrt(((Radius of gyration)^(2))/(Acceleration Due To Gravity*Metacentric height))) GO

Theoretical Maximum Stress for ANC Code Alloy Steel Tubing

Critical stress=135000-(15.9/End Fixity Coefficient)*((Length/Radius of gyration)^2) GO

Theoretical Maximum Stress for ANC Code 2017ST Aluminium

Critical stress=34500-(245/sqrt(End Fixity Coefficient))*(Length/Radius of gyration) GO

Theoretical Maximum Stress for ANC Code Spruce

Critical stress=5000-(0.5/End Fixity Coefficient)*((Length/Radius of gyration)^2) GO

Minimum periodic time of SHM for compound pendulum

Time Period SHM=2*pi*sqrt(2*Radius of gyration/Acceleration Due To Gravity) GO

Length of a Rectangular Section Under Compression

Length=3*Distance from nearest Edge GO

< 5 Other formulas that calculate the same Output

Maximum unit stress in the steel

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

Maximum Stress For Short Beams

Maximum stress at crack tip=(Axial Load/Cross sectional area)+((Maximum Bending Moment*Distance from the Neutral axis)/Moment of Inertia) GO

The maximum stress in the bottom flange

Maximum stress at crack tip= (Dead Load Moment+Live Load Moment)/ Section Modulus of Transformed Composite Section GO

Maximum Stress For a Rectangular Section Under Compression

Maximum stress at crack tip=(2/3)*Concentrated load/(Height of cross section*Distance from nearest Edge) GO

Maximum stress at crack tip

Maximum stress at crack tip=Stress concentration factor*Applied stress GO

Maximum Stress For a Circular Section Under Compression Formula

Maximum stress at crack tip=(0.372+0.056*(Distance from nearest Edge/Radius of gyration)*(Concentrated load/Distance from nearest Edge)*sqrt(Radius of gyration*Distance from nearest Edge))
σm=(0.372+0.056*(k/kG)*(P/k)*sqrt(kG*k))

More formulas

Maximum Stress For a Rectangular Cross Section GO

Maximum Stress For a Circular Cross Section GO

Theoretical Maximum Stress for ANC Code Alloy Steel Tubing GO

Theoretical Maximum Stress for ANC Code 2017ST Aluminium GO

Theoretical Maximum Stress for ANC Code Spruce GO

Theoretical Maximum Stress for Johnson Code Steels GO

Theoretical Maximum Stress for Secant Code Steels GO

Length of a Rectangular Section Under Compression GO

Maximum Stress For a Rectangular Section Under Compression GO

Radius of the Kern for a Circular Ring GO

Radius of the Kern for a Hollow Square GO

Thickness of Wall for a Hollow Octagon GO

Compressive stress

Compressive stress is a force that causes a material to deform to occupy a smaller volume. When a material is experiencing a compressive stress, it is said to be under compression.

How to Calculate Maximum Stress For a Circular Section Under Compression?

Maximum Stress For a Circular Section Under Compression calculator uses Maximum stress at crack tip=(0.372+0.056*(Distance from nearest Edge/Radius of gyration)*(Concentrated load/Distance from nearest Edge)*sqrt(Radius of gyration*Distance from nearest Edge)) to calculate the Maximum stress at crack tip, The Maximum Stress For a Circular Section Under Compression formula is defined as the dimension of Circular section under compressive loading. Maximum stress at crack tip and is denoted by σ_m symbol.

How to calculate Maximum Stress For a Circular Section Under Compression using this online calculator? To use this online calculator for Maximum Stress For a Circular Section Under Compression, enter Distance from nearest Edge (k), Radius of gyration (k_G) and Concentrated load (P) and hit the calculate button. Here is how the Maximum Stress For a Circular Section Under Compression calculation can be explained with given input values -> 1.088E-6 = (0.372+0.056*(19.6133/3)*(5/19.6133)*sqrt(3*19.6133)).

FAQ

What is Maximum Stress For a Circular Section Under Compression?

The Maximum Stress For a Circular Section Under Compression formula is defined as the dimension of Circular section under compressive loading and is represented as σ_m=(0.372+0.056*(k/k_G)*(P/k)*sqrt(k_G*k)) or Maximum stress at crack tip=(0.372+0.056*(Distance from nearest Edge/Radius of gyration)*(Concentrated load/Distance from nearest Edge)*sqrt(Radius of gyration*Distance from nearest Edge)). Distance from nearest Edge is the distance beatween the closest edge of sections and a point load acting on same section, Radius of gyration or gyradius of a body about an axis of rotation is defined as the radial distance to a point which would have a moment of inertia the same as the body's actual distribution of mass, if the total mass of the body were concentrated there and Concentrated load is a load acting at a single point.

How to calculate Maximum Stress For a Circular Section Under Compression?

The Maximum Stress For a Circular Section Under Compression formula is defined as the dimension of Circular section under compressive loading is calculated using Maximum stress at crack tip=(0.372+0.056*(Distance from nearest Edge/Radius of gyration)*(Concentrated load/Distance from nearest Edge)*sqrt(Radius of gyration*Distance from nearest Edge)). To calculate Maximum Stress For a Circular Section Under Compression, you need Distance from nearest Edge (k), Radius of gyration (k_G) and Concentrated load (P). With our tool, you need to enter the respective value for Distance from nearest Edge, Radius of gyration and Concentrated load 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 stress at crack tip?

In this formula, Maximum stress at crack tip uses Distance from nearest Edge, Radius of gyration and Concentrated load. We can use 5 other way(s) to calculate the same, which is/are as follows -

Maximum stress at crack tip=Stress concentration factor*Applied stress
Maximum stress at crack tip=(Axial Load/Cross sectional area)+((Maximum Bending Moment*Distance from the Neutral axis)/Moment of Inertia)
Maximum stress at crack tip=(2/3)*Concentrated load/(Height of cross section*Distance from nearest Edge)
Maximum stress at crack tip= (Dead Load Moment/Section Modulus of Steel Beam)+(Live Load Moment/Section Modulus of Transformed Composite Section)
Maximum stress at crack tip= (Dead Load Moment+Live Load Moment)/ Section Modulus of Transformed Composite Section

Facebook
Twitter
WhatsApp
Reddit
LinkedIn
E-Mail

Let Others Know

✖

Facebook

Twitter

Copied!