Mridul Sharma
Indian Institute of Information Technology (IIIT), Bhopal
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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

Allowable Compression Stress when Slenderness Ratio is less than Cc
allowable compression stress=(1-((Slenderness Ratio^2)/(2*Value of Cc^2)))/((5/3)+(3*Slenderness Ratio/(8*Value of Cc))-((Slenderness Ratio^3)/(8*(Value of Cc^3))))*minimum specified yield stress of steel GO
Safety Factor for Allowable Compressive Stress
Safety factor=5/3+0.375*(Slenderness Ratio/Slenderness ratio for separation)-(0.125*(Slenderness Ratio/Slenderness ratio for separation)^3) GO
Coefficient of pressure with slenderness ratio
Pressure coefficient=2*(Slenderness Ratio^2)*(Non-dimensionalized Pressure-(1/(Specific Heat Ratio*(Mach Number^2)*(Slenderness Ratio^2)))) GO
Non dimensional Change in hypersonic disturbance velocity in x direction
Non dimensional disturbance x velocity=Change in velocity for hypersonic flow/(Freestream Velocity*Slenderness Ratio^2) GO
Slenderness Ratio that Demarcates Between Inelastic from Elastic Buckling
Slenderness Ratio=sqrt(2*(pi^2)*elastic modulus of steel*minimum specified yield stress of steel) GO
Cross-Sectional Area when Critical Buckling Load for Pin Ended Columns is Given
Cross sectional area=Critical Buckling Load*(Slenderness Ratio^2)/((pi^2)*Young's Modulus) GO
Transformed conical variable
Transformed conical variable=Radius of cone/(Slenderness Ratio*Height of Cone) GO
Non dimensional radius for hypersonic vehicles
Non dimensionalized radius=Radius of cone/(Slenderness Ratio*Height of Cone) GO
Similarity constant equation with slenderness ratio
Hypersonic similarity parameter=Mach Number*Slenderness Ratio GO
Allowable Compressive Stress when Slenderness Ration is Greater than Cc
Allowable compressive stress=150000/(Slenderness Ratio)^2 GO
Transformed conical variable with wave angle
Transformed conical variable=Wave angle/Slenderness Ratio GO

1 Other formulas that calculate the same Output

Allowable Compression Stress when Slenderness Ratio is less than Cc
allowable compression stress=(1-((Slenderness Ratio^2)/(2*Value of Cc^2)))/((5/3)+(3*Slenderness Ratio/(8*Value of Cc))-((Slenderness Ratio^3)/(8*(Value of Cc^3))))*minimum specified yield stress of steel GO

Allowable Compression Stress when Slenderness Ratio is Greater than Cc Formula

allowable compression stress=(12*(pi^2)*elastic modulus of steel)/(23*(Slenderness Ratio^2))
F<sub>a</sub>=(12*(pi^2)*E)/(23*(λ ^2))
More formulas
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

What is Allowable Compression Stress?

The allowable stress or allowable strength is the maximum stress (tensile, compressive or bending) that is allowed to be applied on a structural material.

How to Calculate Allowable Compression Stress when Slenderness Ratio is Greater than Cc?

Allowable Compression Stress when Slenderness Ratio is Greater than Cc calculator uses allowable compression stress=(12*(pi^2)*elastic modulus of steel)/(23*(Slenderness Ratio^2)) to calculate the allowable compression stress, The Allowable Compression Stress when Slenderness Ratio is Greater than Cc formula calculates the LOWER OF maximum compression stress when it is known that slenderness ratio is more than Cc. allowable compression stress and is denoted by Fa symbol.

How to calculate Allowable Compression Stress when Slenderness Ratio is Greater than Cc using this online calculator? To use this online calculator for Allowable Compression Stress when Slenderness Ratio is Greater than Cc, enter elastic modulus of steel (E) and Slenderness Ratio (λ ) and hit the calculate button. Here is how the Allowable Compression Stress when Slenderness Ratio is Greater than Cc calculation can be explained with given input values -> 5.973E-5 = (12*(pi^2)*29000)/(23*(50^2)).

FAQ

What is Allowable Compression Stress when Slenderness Ratio is Greater than Cc?
The Allowable Compression Stress when Slenderness Ratio is Greater than Cc formula calculates the LOWER OF maximum compression stress when it is known that slenderness ratio is more than Cc and is represented as Fa=(12*(pi^2)*E)/(23*(λ ^2)) or allowable compression stress=(12*(pi^2)*elastic modulus of steel)/(23*(Slenderness Ratio^2)). elastic modulus of steel also known as modulus of elasticity of steel is 200 GPa (29,000,000 psi) and The Slenderness ratio is the ratio of the length of a column and the least radius of gyration of its cross section.
How to calculate Allowable Compression Stress when Slenderness Ratio is Greater than Cc?
The Allowable Compression Stress when Slenderness Ratio is Greater than Cc formula calculates the LOWER OF maximum compression stress when it is known that slenderness ratio is more than Cc is calculated using allowable compression stress=(12*(pi^2)*elastic modulus of steel)/(23*(Slenderness Ratio^2)). To calculate Allowable Compression Stress when Slenderness Ratio is Greater than Cc, you need elastic modulus of steel (E) and Slenderness Ratio (λ ). With our tool, you need to enter the respective value for elastic modulus of steel and Slenderness Ratio 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 allowable compression stress?
In this formula, allowable compression stress uses elastic modulus of steel and Slenderness Ratio. We can use 1 other way(s) to calculate the same, which is/are as follows -
  • allowable compression stress=(1-((Slenderness Ratio^2)/(2*Value of Cc^2)))/((5/3)+(3*Slenderness Ratio/(8*Value of Cc))-((Slenderness Ratio^3)/(8*(Value of Cc^3))))*minimum specified yield stress of steel
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