Chandana P Dev
NSS College of Engineering (NSSCE), Palakkad
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Ishita Goyal
Meerut Institute of Engineering and Technology (MIET), Meerut
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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 y direction
Non dimensional disturbance y velocity=Change in velocity for hypersonic flow y direction/(Freestream Velocity*Slenderness Ratio) 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
Allowable Compression Stress when Slenderness Ratio is Greater than Cc
allowable compression stress=(12*(pi^2)*elastic modulus of steel)/(23*(Slenderness Ratio^2)) 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
Transformed conical variable with wave angle
Transformed conical variable=Wave angle/Slenderness Ratio GO

1 Other formulas that calculate the same Output

Allowable Compressive Stress when Slenderness Ratio is Less than Cc
Allowable compressive stress=(Yield stress of steel/Safety factor)*(1-(((effective length factor*Effective length)/Radius of gyration )^2)/(2*Slenderness ratio for separation^2)) GO

Allowable Compressive Stress when Slenderness Ration is Greater than Cc Formula

Allowable compressive stress=150000/(Slenderness Ratio)^2
F<sub>a</sub>=150000/(λ )^2
More formulas
Slenderness Ratio Used for Separation GO
Allowable Compressive Stress when Slenderness Ratio is Less than Cc GO
Safety Factor for Allowable Compressive Stress GO
Effective Length Factor GO

What is allowable stress design or ASD?

In allowable stress (or working stress) design, member stresses computed under the action of service (or working) loads are compared to some predesignated stresses called allowable stresses. The allowable stresses are usually expressed as a function of the yield stress or tensile stress of the material.

How to Calculate Allowable Compressive Stress when Slenderness Ration is Greater than Cc?

Allowable Compressive Stress when Slenderness Ration is Greater than Cc calculator uses Allowable compressive stress=150000/(Slenderness Ratio)^2 to calculate the Allowable compressive stress, The Allowable Compressive Stress when Slenderness Ration is Greater than Cc formula is defined using the parameters slenderness ratio and modulus of elasticity. . Allowable compressive stress and is denoted by Fa symbol.

How to calculate Allowable Compressive Stress when Slenderness Ration is Greater than Cc using this online calculator? To use this online calculator for Allowable Compressive Stress when Slenderness Ration is Greater than Cc, enter Slenderness Ratio (λ ) and hit the calculate button. Here is how the Allowable Compressive Stress when Slenderness Ration is Greater than Cc calculation can be explained with given input values -> 8.702E-6 = 150000/(50)^2.

FAQ

What is Allowable Compressive Stress when Slenderness Ration is Greater than Cc?
The Allowable Compressive Stress when Slenderness Ration is Greater than Cc formula is defined using the parameters slenderness ratio and modulus of elasticity. and is represented as Fa=150000/(λ )^2 or Allowable compressive stress=150000/(Slenderness Ratio)^2. 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 Compressive Stress when Slenderness Ration is Greater than Cc?
The Allowable Compressive Stress when Slenderness Ration is Greater than Cc formula is defined using the parameters slenderness ratio and modulus of elasticity. is calculated using Allowable compressive stress=150000/(Slenderness Ratio)^2. To calculate Allowable Compressive Stress when Slenderness Ration is Greater than Cc, you need Slenderness Ratio (λ ). With our tool, you need to enter the respective value for 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 compressive stress?
In this formula, Allowable compressive stress uses Slenderness Ratio. We can use 1 other way(s) to calculate the same, which is/are as follows -
  • Allowable compressive stress=(Yield stress of steel/Safety factor)*(1-(((effective length factor*Effective length)/Radius of gyration )^2)/(2*Slenderness ratio for separation^2))
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