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

Category	Engineering ↺
Engineering	Civil ↺
Civil	Surveying Formulas ↺
Surveying-Formulas	Measurement of Distance with Tapes ↺
Measurement-Of-Distance-With-Tapes	Temperature Corrections ↺

✖Pull on Tape is the tension or pull applied to the tape in newtons (N).ⓘ Pull on Tape [P]			+10% -10%
✖Total Tension is the force that tries to elongate a body or an object.ⓘ Total Tension [T]			+10% -10%
✖Unsupported length is the length between the support.ⓘ Unsupported length [L]			+10% -10%
✖The temperature correction to be applied for tempera- ture when using a steel tape.ⓘ Temperature correction [Ct]			+10% -10%
✖The modulus of elasticity of a material is a measure of its stiffnessⓘ Modulus of elasticity [E_s]			+10% -10%

✖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.ⓘ Tape Cross-Sectional Area when Temperature Corrections for Nonstandard Tension is Given [A]

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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 (E_s) 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*E_s) 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 (E_s). 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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