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 300+ more calculators!

11 Other formulas that you can solve using the same Inputs

Moment Resistance of Steel
Moment Resistance of Steel=(Total Tension*Ratio of Distance between centroids *Effective depth of beam)+(area of tension reinforcement*Tensile Stress in Steel*Ratio of Distance between centroids *Effective depth of beam) GO
Tension Correction to Measured Length
Tension correction=(((Final tension-Initial tension)*Measured length)/(Area of tape*Modulus of elasticity)) GO
Tape Standardized Tension when Tension Correction to Measured Length is Given
Initial tension=(Final tension-((Tension correction*Area of tape*Modulus of elasticity)/Measured length)) GO
Actual Tension when Tension Correction to Measured Length is Given
Final tension=(Initial tension+((Tension correction*Area of tape*Modulus of elasticity)/Measured length)) GO
Measured Length when Tension Correction to Measured Length is Given
Measured length=(Tension correction*Area of tape*Modulus of elasticity)/(Final tension-Initial tension) GO
Actual Tension when Sag Correction of Unsupported Tape is Given
Initial tension=(((Weight of tape per unit length^2)*(Unsupported length^3))/(24*Sag correction))^(1/2) GO
Tape Weight when Sag Correction of Unsupported Tape is Given
Weight of tape per unit length=((Sag correction*24*(Initial tension^2))/(Unsupported length^3))^(1/2) GO
Sag Correction of Unsupported Tape
Sag correction=((Weight of tape per unit length^2)*(Unsupported length^3))/(24*(Initial tension^2)) GO
Measured Length when Temperature Correction is Given
Measured length=(Temperature correction/(0.0000065*(final temp.-initial temp.))) GO
Horizontal Offset when Slope Correction for Slopes of 10 Percent or Less is Given
Difference in elevation=(2*Unsupported length*Slope correction)^(1/2) GO
Slope Correction for Slopes of 10 Percent or Less
Slope correction=Difference in elevation^2/(2*Unsupported length) GO

11 Other formulas that calculate the same Output

Cross-Sectional Area When Stress is Applied at Point y in a Curved Beam
Cross sectional area=(Bending Moment /(Stress*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
Cross-Sectional Area when Axial Buckling Load for a Warped Section is Given
Cross sectional area=(Axial buckling Load*Polar moment of Inertia)/(Shear Modulus of Elasticity*Torsion constant+((pi^2)*Young's Modulus*Warping Constant/(Length^2))) GO
Cross-Sectional Area when Total Unit Stress in Eccentric Loading is Given
Cross sectional area=Axial Load/(Total Unit Stress-((Axial Load*Outermost Fiber Distance*Distance_from Load Applied/Moment of Inertia about Neutral Axis))) GO
Cross-sectional area of the rod if stress induced in rod due to impact load is known
Cross sectional area=(2*Modulus Of Elasticity*Load Dropped(Impact Load)*Height through which load is dropped)/(Length of Rod*(Stress induced^2)) GO
Cross-Sectional Area when Elastic Critical Buckling Load is Given
Cross sectional area=(Critical Buckling Load*((Coefficient for Column End Conditions*Length/Radius of gyration)^2))/((pi^2)*Young's Modulus) GO
Cross-Sectional Area when Maximum Stress For Short Beams is Given
Cross sectional area=Axial Load/(Maximum stress at crack tip-(Maximum Bending Moment*Distance from the Neutral axis/Moment of Inertia)) GO
Cross-Sectional Area when Torsional Buckling Load for Pin Ended Columns is Given
Cross sectional area=Torsional buckling load*Polar moment of Inertia/(Shear Modulus of Elasticity*Torsion constant) 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
Cross-sectional Area of Soil Conveying Flow when Rate of Flow of Water is Given
Cross sectional area=(Rate of flow/(Coefficient of permeability*Hydraulic gradient)) GO
Total Cross-Sectional Area of Tensile Reinforcing
Cross sectional area=8*Bending moment/(7*Reinforcement Stress*Depth of the Beam) GO
Area when water flow equation is given
Cross sectional area=water flow/flow velocity GO

Tape Cross-Sectional Area when Temperature Corrections for Nonstandard Tension is Given Formula

Cross sectional area=((Pull on Tape-Total Tension)*Unsupported length)/(Temperature correction*Modulus of elasticity)
A=((P-T)*L)/(Ct*E<sub>s</sub>)
More formulas
Temperature Corrections for Incorrect Tape Length GO
Temperature Corrections for Nonstandard Tension 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 Tape Cross-Sectional Area when Temperature Corrections for Nonstandard Tension is Given?

Tape Cross-Sectional Area when Temperature Corrections for Nonstandard Tension is Given calculator uses Cross sectional area=((Pull on Tape-Total Tension)*Unsupported length)/(Temperature correction*Modulus of elasticity) to calculate the Cross sectional area, The Tape Cross-Sectional Area when Temperature Corrections for Nonstandard Tension is Given formula is defined as . Cross sectional area and is denoted by A symbol.

How to calculate Tape Cross-Sectional Area when Temperature Corrections for Nonstandard Tension is Given using this online calculator? To use this online calculator for Tape Cross-Sectional Area when Temperature Corrections for Nonstandard Tension is Given, enter Pull on Tape (P), Total Tension (T), Unsupported length (L), Temperature correction (Ct) and Modulus of elasticity (Es) and hit the calculate button. Here is how the Tape Cross-Sectional Area when Temperature Corrections for Nonstandard Tension is Given calculation can be explained with given input values -> -4.750E-10 = ((5-100)*10)/(10*200000000000).

FAQ

What is Tape Cross-Sectional Area when Temperature Corrections for Nonstandard Tension is Given?
The Tape Cross-Sectional Area when Temperature Corrections for Nonstandard Tension is Given formula is defined as and is represented as A=((P-T)*L)/(Ct*Es) or Cross sectional area=((Pull on Tape-Total Tension)*Unsupported length)/(Temperature correction*Modulus of elasticity). Pull on Tape is the tension or pull applied to the tape in newtons (N), Total Tension is the force that tries to elongate a body or an object, Unsupported length is the length between the support, The temperature correction to be applied for tempera- ture when using a steel tape and The modulus of elasticity of a material is a measure of its stiffness.
How to calculate Tape Cross-Sectional Area when Temperature Corrections for Nonstandard Tension is Given?
The Tape Cross-Sectional Area when Temperature Corrections for Nonstandard Tension is Given formula is defined as is calculated using Cross sectional area=((Pull on Tape-Total Tension)*Unsupported length)/(Temperature correction*Modulus of elasticity). To calculate Tape Cross-Sectional Area when Temperature Corrections for Nonstandard Tension is Given, you need Pull on Tape (P), Total Tension (T), Unsupported length (L), Temperature correction (Ct) and Modulus of elasticity (Es). With our tool, you need to enter the respective value for Pull on Tape, Total Tension, Unsupported length, Temperature correction 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 Cross sectional area?
In this formula, Cross sectional area uses Pull on Tape, Total Tension, Unsupported length, Temperature correction and Modulus of elasticity. We can use 11 other way(s) to calculate the same, which is/are as follows -
  • Cross sectional area=(Bending Moment /(Stress*Radius of Centroidal Axis))*(1+(Distance of Point from Centroidal Axis/(Cross-Section Property*(Radius of Centroidal Axis+Distance of Point from Centroidal Axis))))
  • Cross sectional area=Axial Load/(Maximum stress at crack tip-(Maximum Bending Moment*Distance from the Neutral axis/Moment of Inertia))
  • Cross sectional area=Axial Load/(Total Unit Stress-((Axial Load*Outermost Fiber Distance*Distance_from Load Applied/Moment of Inertia about Neutral Axis)))
  • Cross sectional area=Critical Buckling Load*(Slenderness Ratio^2)/((pi^2)*Young's Modulus)
  • Cross sectional area=(Critical Buckling Load*((Coefficient for Column End Conditions*Length/Radius of gyration)^2))/((pi^2)*Young's Modulus)
  • Cross sectional area=Torsional buckling load*Polar moment of Inertia/(Shear Modulus of Elasticity*Torsion constant)
  • Cross sectional area=(Axial buckling Load*Polar moment of Inertia)/(Shear Modulus of Elasticity*Torsion constant+((pi^2)*Young's Modulus*Warping Constant/(Length^2)))
  • Cross sectional area=8*Bending moment/(7*Reinforcement Stress*Depth of the Beam)
  • Cross sectional area=(2*Modulus Of Elasticity*Load Dropped(Impact Load)*Height through which load is dropped)/(Length of Rod*(Stress induced^2))
  • Cross sectional area=water flow/flow velocity
  • Cross sectional area=(Rate of flow/(Coefficient of permeability*Hydraulic gradient))
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