Ishita Goyal
Meerut Institute of Engineering and Technology (MIET), Meerut
Ishita Goyal has created this Calculator and 100+ more calculators!
Chandana P Dev
NSS College of Engineering (NSSCE), Palakkad
Chandana P Dev has verified this Calculator and 400+ more calculators!

11 Other formulas that you can solve using the same Inputs

Stress at Point y for a Curved Beam
Stress=((Bending Moment )/(Cross sectional area*Radius of Centroidal Axis))*(1+((Distance of Point from Centroidal Axis)/(Cross-Section Property*(Radius of Centroidal Axis+Distance of Point from Centroidal Axis)))) GO
Bending Moment When Stress is Applied at Point y in a Curved Beam
Bending Moment =((Stress*Cross sectional area*Radius of Centroidal Axis)/(1+(Distance of Point from Centroidal Axis/(Cross-Section Property*(Radius of Centroidal Axis+Distance of Point from Centroidal Axis))))) GO
Neutral Axis to Outermost Fiber Distance when Total Unit Stress in Eccentric Loading is Given
Outermost Fiber Distance=(Total Unit Stress-(Axial Load/Cross sectional area))*Moment of Inertia about Neutral Axis/(Axial Load*Distance_from Load Applied) GO
Total Unit Stress in Eccentric Loading
Total Unit Stress=(Axial Load/Cross sectional area)+(Axial Load*Outermost Fiber Distance*Distance_from Load Applied/Moment of Inertia about Neutral Axis) GO
Maximum Bending Moment when Maximum Stress For Short Beams is Given
Maximum Bending Moment=((Maximum stress at crack tip-(Axial Load/Cross sectional area))*Moment of Inertia)/Distance from the Neutral axis GO
Maximum Stress For Short Beams
Maximum stress at crack tip=(Axial Load/Cross sectional area)+((Maximum Bending Moment*Distance from the Neutral axis)/Moment of Inertia) GO
Axial Load when Maximum Stress For Short Beams is Given
Axial Load=Cross sectional area*(Maximum stress at crack tip-(Maximum Bending Moment*Distance from the Neutral axis/Moment of Inertia)) GO
Electric Current when Drift Velocity is Given
Electric Current=Number of free charge particles per unit volume*[Charge-e]*Cross sectional area*Drift Velocity GO
Resistance
Resistance=(Resistivity*Length of Conductor)/Cross sectional area GO
Centrifugal Stress
Centrifugal Stress=2*Tensile Stress*Cross sectional area GO
Rate of Flow
Rate of flow=Cross sectional area*Average Velocity GO

2 Other formulas that calculate the same Output

Temperature Corrections for Incorrect Tape Length
Temperature correction=((actual tape length-nominal tape length)*Unsupported length)/(nominal tape length) GO
Temperature Correction to Measured Length
Temperature correction=(0.0000065*Measured length*(Final temperature-Initial temperature)) GO

Temperature Corrections for Nonstandard Tension Formula

Temperature correction=((Pull on Tape-Final tension)*Unsupported length)/(Cross sectional area*Modulus of elasticity)
Ct=((P-P<sub>f</sub>)*L)/(A*E<sub>s</sub>)
More formulas
Temperature Corrections for Incorrect Tape Length GO
Tape Cross-Sectional Area when Temperature Corrections for Nonstandard Tension is Given GO
Sag Correction Between Points of Support GO
Tape Weight per Foot when Sag Correction Between Points of Support is Given GO
Unsupported Tape Length when Sag Correction Between Points of Support is Given GO
Pull on Tape when Sag Correction Between Points of Support is Given GO

What is tension?

Tension is applied to a tape to compensate for the shortening effect of the sag of the tape in order to bring the tape to standard length.

How to Calculate Temperature Corrections for Nonstandard Tension?

Temperature Corrections for Nonstandard Tension calculator uses Temperature correction=((Pull on Tape-Final tension)*Unsupported length)/(Cross sectional area*Modulus of elasticity) to calculate the Temperature correction, The Temperature Corrections for Nonstandard Tension formula is defined as the corrections which are applied to tape due to the pull exerted on it. Temperature correction and is denoted by Ct symbol.

How to calculate Temperature Corrections for Nonstandard Tension using this online calculator? To use this online calculator for Temperature Corrections for Nonstandard Tension, enter Pull on Tape (P), Final tension (Pf), Unsupported length (L), Cross sectional area (A) and Modulus of elasticity (Es) and hit the calculate button. Here is how the Temperature Corrections for Nonstandard Tension calculation can be explained with given input values -> -2.500E-11 = ((5-10)*10)/(10*200000000000).

FAQ

What is Temperature Corrections for Nonstandard Tension?
The Temperature Corrections for Nonstandard Tension formula is defined as the corrections which are applied to tape due to the pull exerted on it and is represented as Ct=((P-Pf)*L)/(A*Es) or Temperature correction=((Pull on Tape-Final tension)*Unsupported length)/(Cross sectional area*Modulus of elasticity). Pull on Tape is the tension or pull applied to the tape in newtons (N), The final tension is the actual tension applied during observation, Unsupported length is the length between the support, Cross sectional area is the area of a two-dimensional shape that is obtained when a three dimensional shape is sliced perpendicular to some specifies axis at a point and The modulus of elasticity of a material is a measure of its stiffness.
How to calculate Temperature Corrections for Nonstandard Tension?
The Temperature Corrections for Nonstandard Tension formula is defined as the corrections which are applied to tape due to the pull exerted on it is calculated using Temperature correction=((Pull on Tape-Final tension)*Unsupported length)/(Cross sectional area*Modulus of elasticity). To calculate Temperature Corrections for Nonstandard Tension, you need Pull on Tape (P), Final tension (Pf), Unsupported length (L), Cross sectional area (A) and Modulus of elasticity (Es). With our tool, you need to enter the respective value for Pull on Tape, Final tension, Unsupported length, Cross sectional area and Modulus of elasticity 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 Temperature correction?
In this formula, Temperature correction uses Pull on Tape, Final tension, Unsupported length, Cross sectional area and Modulus of elasticity. We can use 2 other way(s) to calculate the same, which is/are as follows -
  • Temperature correction=(0.0000065*Measured length*(Final temperature-Initial temperature))
  • Temperature correction=((actual tape length-nominal tape length)*Unsupported length)/(nominal tape length)
Share Image
Let Others Know
Facebook
Twitter
Reddit
LinkedIn
Email
WhatsApp
Copied!