Magnified Moment when Eccentricity of Slender Columns is Given Calculator

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✖Eccentricity of an ellipse is a non-negative real number that uniquely characterizes its shape.ⓘ Eccentricity [e]			+10% -10%
✖Axial Load Capacity is defined as the maximum load along the direction of the drive train.ⓘ Axial Load Capacity [P_u]			+10% -10%

✖Magnified moment is a simplified way of accounting for column slenderness effects by doing a P-Delta analysis of the frame.ⓘ Magnified Moment when Eccentricity of Slender Columns is Given [M_c]

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Magnified Moment when Eccentricity of Slender Columns is Given

Rudrani Tidke

Cummins College of Engineering for Women (CCEW), Pune

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

Mridul Sharma

Indian Institute of Information Technology (IIIT), Bhopal

Mridul Sharma has verified this Calculator and 200+ more calculators!

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

Tension Reinforcement Area when Axial-Load Capacity of Short Rectangular Members is Given

area of tension reinforcement=((.85*28 Day Compressive Strength of Concrete*Width of compression face*Depth Rectangular Compressive Stress)+(Area of Compressive Reinforcement*Yeild Strength of Base Plate)-(Axial Load Capacity/Resistance Factor))/Tensile Stress in Steel GO

Tensile Stress in Steel when Axial-Load Capacity of Short Rectangular Members is Given

Tensile Stress in Steel=((.85*28 Day Compressive Strength of Concrete*Width of compression face*Depth Rectangular Compressive Stress)+(Area of Compressive Reinforcement*Yeild Strength of Base Plate)-(Axial Load Capacity/Resistance Factor))/area of tension reinforcement 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

Maximum Stress For a Circular Cross Section

Maximum stress for a section=Axial Stress*(1+8*Eccentricity/Diameter ) GO

Maximum Stress For a Rectangular Cross Section

Maximum stress for a section=Axial Stress*(1+6*Eccentricity/Width) GO

Latus rectum of an ellipse when focal parameter is given

Latus Rectum=Focal parameter of an ellipse*Eccentricity GO

Semi-latus rectum of an ellipse when eccentricity is given

Semi-latus rectum=Semi-major axis*(1-(Eccentricity)^2) GO

Linear eccentricity of an ellipse when eccentricity and semimajor axis are given

Linear Eccentricity=(Eccentricity*Semi-major axis) GO

Linear eccentricity of ellipse when eccentricity and major axis are given

Linear Eccentricity=Eccentricity*Major axis GO

Directrix of an ellipse(a>b)

Directrix=Major axis/Eccentricity GO

Directrix of an ellipse(b>a)

Directrix=Major axis/Eccentricity GO

Magnified Moment when Eccentricity of Slender Columns is Given Formula

Magnified moment=Eccentricity*Axial Load Capacity
M<sub>c</sub>=e*P<sub>u

More formulas

Column Ultimate Strength with Zero Eccentricity of Load GO

Yield Strength of Reinforcing Steel when Column Ultimate Strength is Given GO

28-day Concrete Compressive Strength when Column Ultimate Strength is Given GO

Axial-Load Capacity of Short Rectangular Members GO

Tensile Stress in Steel when Axial-Load Capacity of Short Rectangular Members is Given GO

Tension Reinforcement Area when Axial-Load Capacity of Short Rectangular Members is Given GO

Compressive Reinforcement Area when Axial-Load Capacity of Short Rectangular Members is Given GO

Balanced Moment when Load and Eccentricity is Given GO

Balanced Moment when Φ is Given GO

Ultimate Strength for Symmetrical Reinforcement GO

Ultimate Strength for No Compression Reinforcement GO

Ultimate Strength for Symmetrical Reinforcement in Single Layers GO

Ultimate Strength for Short, Circular Members when Controlled by Tension GO

Ultimate Strength for Short, Circular Members when Governed by Compression GO

Eccentricity for Balanced Condition for Short, Circular Members GO

Ultimate Strength for Short, Square Members when Governed by Compression GO

Ultimate Strength for Short, Square Members when Controlled by Tension GO

Eccentricity of Slender Columns GO

What is Moment magnification?

The provisions in the moment magnification procedure allow for a column to be designed using a conventional first order analysis provided that the moments calculated by the analysis are increased to account for second order effects.

How to Calculate Magnified Moment when Eccentricity of Slender Columns is Given?

Magnified Moment when Eccentricity of Slender Columns is Given calculator uses Magnified moment=Eccentricity*Axial Load Capacity to calculate the Magnified moment, The Magnified Moment when Eccentricity of Slender Columns is Given formula is defined as a simplified way of accounting for column slenderness effects by doing a P-Delta analysis of the frame. Magnified moment and is denoted by M_c symbol.

How to calculate Magnified Moment when Eccentricity of Slender Columns is Given using this online calculator? To use this online calculator for Magnified Moment when Eccentricity of Slender Columns is Given, enter Eccentricity (e) and Axial Load Capacity (P_u) and hit the calculate button. Here is how the Magnified Moment when Eccentricity of Slender Columns is Given calculation can be explained with given input values -> 10 = 0.1*100.

FAQ

What is Magnified Moment when Eccentricity of Slender Columns is Given?

The Magnified Moment when Eccentricity of Slender Columns is Given formula is defined as a simplified way of accounting for column slenderness effects by doing a P-Delta analysis of the frame and is represented as M_c=e*P_u or Magnified moment=Eccentricity*Axial Load Capacity. Eccentricity of an ellipse is a non-negative real number that uniquely characterizes its shape and Axial Load Capacity is defined as the maximum load along the direction of the drive train.

How to calculate Magnified Moment when Eccentricity of Slender Columns is Given?

The Magnified Moment when Eccentricity of Slender Columns is Given formula is defined as a simplified way of accounting for column slenderness effects by doing a P-Delta analysis of the frame is calculated using Magnified moment=Eccentricity*Axial Load Capacity. To calculate Magnified Moment when Eccentricity of Slender Columns is Given, you need Eccentricity (e) and Axial Load Capacity (P_u). With our tool, you need to enter the respective value for Eccentricity and Axial Load Capacity 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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