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
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11 Other formulas that you can solve using the same Inputs

Surface Area of a Rectangular Prism
Surface Area=2*(Length*Width+Length*Height+Width*Height) GO
Perimeter of a rectangle when diagonal and length are given
Perimeter=2*(Length+sqrt((Diagonal)^2-(Length)^2)) GO
Magnetic Flux
Magnetic Flux=Magnetic Field*Length*Breadth*cos(θ) GO
Diagonal of a Rectangle when length and area are given
Diagonal=sqrt(((Area)^2/(Length)^2)+(Length)^2) GO
Area of a Rectangle when length and diagonal are given
Area=Length*(sqrt((Diagonal)^2-(Length)^2)) GO
Diagonal of a Rectangle when length and breadth are given
Diagonal=sqrt(Length^2+Breadth^2) GO
Strain
Strain=Change In Length/Length GO
Surface Tension
Surface Tension=Force/Length GO
Perimeter of a rectangle when length and width are given
Perimeter=2*Length+2*Width GO
Volume of a Rectangular Prism
Volume=Width*Height*Length GO
Area of a Rectangle when length and breadth are given
Area=Length*Breadth GO

5 Other formulas that calculate the same Output

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
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
Critical stress for crack propagation
Critical stress=sqrt(2*Young's Modulus*Specific surface energy/(pi*Crack Length)) GO

Theoretical Maximum Stress for ANC Code Spruce Formula

Critical stress=5000-(0.5/End Fixity Coefficient)*((Length/Radius of gyration)^2)
σ<sub>c</sub>=5000-(0.5/c)*((l/k<sub>G</sub>)^2)
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 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
Thickness of Wall for a Hollow Octagon GO

What is the stress?

Stress is defined as the resistance force acting per unit cross-section area of the body. It is also defined as the ratio of applied load to the cross section area of the body.

How to Calculate Theoretical Maximum Stress for ANC Code Spruce?

Theoretical Maximum Stress for ANC Code Spruce calculator uses Critical stress=5000-(0.5/End Fixity Coefficient)*((Length/Radius of gyration)^2) to calculate the Critical stress, The Theoretical Maximum Stress for ANC Code Spruce formula is defined as maximum possible stress a perfect solid can withstand, when short blocks or short column are loaded eccentrically in compression or in tension (not through the center of gravity). Critical stress and is denoted by σc symbol.

How to calculate Theoretical Maximum Stress for ANC Code Spruce using this online calculator? To use this online calculator for Theoretical Maximum Stress for ANC Code Spruce, enter End Fixity Coefficient (c), Length (l) and Radius of gyration (kG) and hit the calculate button. Here is how the Theoretical Maximum Stress for ANC Code Spruce calculation can be explained with given input values -> 0.005 = 5000-(0.5/1)*((3/3)^2).

FAQ

What is Theoretical Maximum Stress for ANC Code Spruce?
The Theoretical Maximum Stress for ANC Code Spruce formula is defined as maximum possible stress a perfect solid can withstand, when short blocks or short column are loaded eccentrically in compression or in tension (not through the center of gravity) and is represented as σc=5000-(0.5/c)*((l/kG)^2) or Critical stress=5000-(0.5/End Fixity Coefficient)*((Length/Radius of gyration)^2). The end fixity coefficient is defined as the ratio of the moment at one end to the moment at the same end when both the ends are ideally fixed, Length is the measurement or extent of something from end to end and 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.
How to calculate Theoretical Maximum Stress for ANC Code Spruce?
The Theoretical Maximum Stress for ANC Code Spruce formula is defined as maximum possible stress a perfect solid can withstand, when short blocks or short column are loaded eccentrically in compression or in tension (not through the center of gravity) is calculated using Critical stress=5000-(0.5/End Fixity Coefficient)*((Length/Radius of gyration)^2). To calculate Theoretical Maximum Stress for ANC Code Spruce, you need End Fixity Coefficient (c), Length (l) and Radius of gyration (kG). With our tool, you need to enter the respective value for End Fixity Coefficient, Length and Radius of gyration 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 Critical stress?
In this formula, Critical stress uses End Fixity Coefficient, Length and Radius of gyration. We can use 5 other way(s) to calculate the same, which is/are as follows -
  • Critical stress=sqrt(2*Young's Modulus*Specific surface energy/(pi*Crack Length))
  • Critical stress=135000-(15.9/End Fixity Coefficient)*((Length/Radius of gyration)^2)
  • Critical stress=34500-(245/sqrt(End Fixity Coefficient))*(Length/Radius of gyration)
  • 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))
  • 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))))))
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