Rudrani Tidke
Cummins College of Engineering for Women (CCEW), Pune
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Kethavath Srinath
Osmania University (OU), Hyderabad
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11 Other formulas that you can solve using the same Inputs

Concrete Compressive Strength when Total Allowable Axial Load is Given
Compressive strength=((Allowable Load/Gross area of column)-Allowable stress in vertical reinforcement*Area ratio of cross sectional area to gross area)/0.25 Go
Allowable Stress in Vertical Concrete Reinforcing when Total Allowable Axial Load is Given
Allowable stress in vertical reinforcement=(Allowable Load/Gross area of column-0.25*Compressive strength)/Area ratio of cross sectional area to gross area Go
Gross Cross-Sectional Area of Column when Total Allowable Axial Load is Given
Gross area of column=Allowable Load/(0.25*Compressive strength+Allowable stress in vertical reinforcement*Area ratio of cross sectional area to gross area) Go
Radius of Gyration for Single Curvature Bent Member when Load Reduction Factor is Given
Radius of gyration of gross concrete area=1.07-(0.008*Length of column/Long column load reduction factor) Go
Critical Slenderness Ratio for Aluminium Columns
Slenderness Ratio=sqrt(51000000/(Allowable Load/Cross sectional area)) Go
Critical Slenderness Ratio for Cast Iron Columns
Slenderness Ratio=(12000-(Allowable Load/Cross sectional area))/60 Go
Shaft Resistance when Allowable Load and Safety Factor is Given
Shaft Resistance=Factor of Safety*Allowable Load-Toe Resistance Go
Toe Resistance when Allowable Load and Safety Factor is Given
Toe Resistance=Allowable Load*Factor of Safety-Shaft Resistance Go
Smallest Moment of Inertia Allowable at Worst Section for Wrought Iron
Area Moment Of Inertia=Allowable Load*(Length of column^2) Go
Smallest Moment of Inertia Allowable at Worst Section for Medium Carbon Steel
Moment of Inertia=Allowable Load*(Length of column^2) Go
Smallest Moment of Inertia Allowable at Worst Section for Cast Iron
Moment of Inertia=Allowable Load*(Length of column^2) Go

11 Other formulas that calculate the same Output

Moment of Inertia when Strain Energy in Bending is Given
Moment of Inertia=Length*(Bending moment^2)/(2*Strain Energy*Modulus Of Elasticity) Go
Moment of inertia of pickering governor cross-section about the neutral axis
Moment of Inertia=(Width of spring*Thickness of spring^3)/12 Go
Smallest Moment of Inertia Allowable at Worst Section for Cast Iron
Moment of Inertia=Allowable Load*(Length of column^2) Go
Moment of inertia of bob of pendulum, about an axis through the point of suspension
Moment of Inertia=Mass*(Length of the string^2) Go
Moment of Inertia of a rod about an axis through its center of mass and perpendicular to rod
Moment of Inertia=(Mass*(Length of rod^2))/12 Go
Moment of Inertia of a solid sphere about its diameter
Moment of Inertia=2*(Mass*(Radius 1^2))/5 Go
Moment of inertia of a circular disc about an axis through its center and perpendicular to its plane
Moment of Inertia=(Mass*(Radius 1^2))/2 Go
Moment of Inertia of a right circular solid cylinder about its symmetry axis
Moment of Inertia=(Mass*(Radius 1^2))/2 Go
Moment of Inertia of a spherical shell about its diameter
Moment of Inertia=2*(Mass*(Radius 1))/3 Go
Moment of Inertia of a right circular hollow cylinder about its axis
Moment of Inertia=(Mass*(Radius 1)^2) Go
Moment of inertia of a circular ring about an axis through its center and perpendicular to its plane
Moment of Inertia=Mass*(Radius 1^2) Go

Smallest Moment of Inertia Allowable at Worst Section for Low Carbon Steel Formula

Moment of Inertia=Allowable Load*(Length of column^2)
I=Q <sub>a</sub>*(l^2)
More formulas
Euler's Formula for Critical Buckling Load Go
Euler's Formula for Critical Buckling Load when Area is Given Go
Smallest Moment of Inertia Allowable at Worst Section for Cast Iron Go
Smallest Moment of Inertia Allowable at Worst Section for Wrought Iron Go
Smallest Moment of Inertia Allowable at Worst Section for Medium Carbon Steel Go
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 Circular 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
Critical Slenderness Ratio for Cast Iron Columns Go
Ultimate Load per Area for Cast Iron Columns Go
Ultimate Load per Area for Aluminium Columns Go
Ultimate Load per Area for Aluminium Columns Go
Critical Slenderness Ratio for Aluminium Columns Go
Specified Compressive Strength of Concrete when Nominal Bearing Strength is Given Go
Nominal Bearing Strength of the Concrete Go
Area of the Base Plate when Nominal Bearing Strength is Given Go
Area of the Supporting Concrete when Nominal Bearing Strength is Given Go
Required Area of a Base Plate for a Factored Load Go
Factored Load when Base Plate Area is Given Go
Width Parallel to the Flanges Go
Base Plate Thickness when Projection of Base Plate Beyond the Flange and Parallel to Web is Given Go
Base Plate Thickness when Projection of Base Plate Beyond Flange and Perpendicular to Web is Given Go
Projection of Base Plate Beyond the Flange and Parallel to Web Go
Projection of Base Plate Beyond the Flange and Perpendicular to Web Go
Thickness of Wall for a Hollow Octagon Go
Area of foundation of the Lowest Column of a Structure Go
Load when Area of Lowest Column of a Structure is Given Go
Allowable Bearing Pressure when Area of Lowest Column of a Structure is Given Go
Allowable Bearing Pressure when Full Area of Support is Occupied by Base Plate Go
Equivalent Cantilever Dimension Go
Base Plate Thickness Go
Design Strength of an Axially Loaded Composite Column Go
Gross Area of Steel Core when Design Strength of Axially Loaded Composite Column is Given Go
Design Strength of Concrete for Direct Bearing Go
Loaded Area when Design Strength of Concrete for Direct Bearing is Given Go
Critical Buckling Load for Pin Ended Columns Go
Slenderness Ratio of when Critical Buckling Load for Pin Ended Columns is Given Go
Cross-Sectional Area when Critical Buckling Load for Pin Ended Columns is Given Go
Elastic Critical Buckling Load Go
Cross-Sectional Area when Elastic Critical Buckling Load is Given Go
Radius of Gyration of Column when Elastic Critical Buckling Load is Given Go
Torsional Buckling Load for Pin Ended Columns Go
Cross-Sectional Area when Torsional Buckling Load for Pin Ended Columns is Given Go
Polar Moment of Inertia for Pin Ended Columns Go
Axial Buckling Load for a Warped Section Go
Cross-Sectional Area when Axial Buckling Load for a Warped Section is Given Go
Polar Moment of Inertia when Axial Buckling Load for a Warped Section is Given Go
Radius of Gyration of Column when Allowable Compressive Stress for Aluminium Columns is Given Go
Length of Column when Allowable Compressive Stress for Aluminium Columns is Given Go
Allowable Compressive Stress for Aluminium Columns Go
Allowable Compressive Stress for Aluminium Columns when Column Yield Stress is Given Go
Transition from Long to Short Column Range Go
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
Magnified Moment when Eccentricity of Slender Columns is Given Go
Eccentricity of Slender Columns Go
LRFD Strength for a Compression Member Go
LRFD Design Strength of Member Go
Slenderness Ratio that Demarcates Between Inelastic from Elastic Buckling Go
Allowable Compression Stress when Slenderness Ratio is less than Cc Go
Allowable Compression Stress when Slenderness Ratio is Greater than Cc Go

Define Rotational Inertia?

Rotational inertia is also commonly known as moment of inertia. It is also sometimes called the second moment of mass; the 'second' here refers to the fact that it depends on the length of the moment arm squared.

How to Calculate Smallest Moment of Inertia Allowable at Worst Section for Low Carbon Steel?

Smallest Moment of Inertia Allowable at Worst Section for Low Carbon Steel calculator uses Moment of Inertia=Allowable Load*(Length of column^2) to calculate the Moment of Inertia, Smallest Moment of Inertia Allowable at Worst Section for Low Carbon Steel formula is defined as the quantity expressed by the body resisting angular acceleration which is the sum of the product of the mass of every particle with its square of a distance from the axis of rotation. Moment of Inertia and is denoted by I symbol.

How to calculate Smallest Moment of Inertia Allowable at Worst Section for Low Carbon Steel using this online calculator? To use this online calculator for Smallest Moment of Inertia Allowable at Worst Section for Low Carbon Steel, enter Allowable Load (Q a) and Length of column (l) and hit the calculate button. Here is how the Smallest Moment of Inertia Allowable at Worst Section for Low Carbon Steel calculation can be explained with given input values -> 250000 = 10000*(5^2).

FAQ

What is Smallest Moment of Inertia Allowable at Worst Section for Low Carbon Steel?
Smallest Moment of Inertia Allowable at Worst Section for Low Carbon Steel formula is defined as the quantity expressed by the body resisting angular acceleration which is the sum of the product of the mass of every particle with its square of a distance from the axis of rotation and is represented as I=Q a*(l^2) or Moment of Inertia=Allowable Load*(Length of column^2). Allowable load is the maximum working load that can be applied on the structure and Length of column is the distance between two points where a column gets its fixity of support so its movement is restrained in all directions.
How to calculate Smallest Moment of Inertia Allowable at Worst Section for Low Carbon Steel?
Smallest Moment of Inertia Allowable at Worst Section for Low Carbon Steel formula is defined as the quantity expressed by the body resisting angular acceleration which is the sum of the product of the mass of every particle with its square of a distance from the axis of rotation is calculated using Moment of Inertia=Allowable Load*(Length of column^2). To calculate Smallest Moment of Inertia Allowable at Worst Section for Low Carbon Steel, you need Allowable Load (Q a) and Length of column (l). With our tool, you need to enter the respective value for Allowable Load and Length of column 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 Moment of Inertia?
In this formula, Moment of Inertia uses Allowable Load and Length of column. We can use 11 other way(s) to calculate the same, which is/are as follows -
  • Moment of Inertia=(Mass*(Length of rod^2))/12
  • Moment of Inertia=Mass*(Radius 1^2)
  • Moment of Inertia=(Mass*(Radius 1^2))/2
  • Moment of Inertia=(Mass*(Radius 1^2))/2
  • Moment of Inertia=(Mass*(Radius 1)^2)
  • Moment of Inertia=2*(Mass*(Radius 1^2))/5
  • Moment of Inertia=2*(Mass*(Radius 1))/3
  • Moment of Inertia=Mass*(Length of the string^2)
  • Moment of Inertia=(Width of spring*Thickness of spring^3)/12
  • Moment of Inertia=Length*(Bending moment^2)/(2*Strain Energy*Modulus Of Elasticity)
  • Moment of Inertia=Allowable Load*(Length of column^2)
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