🔍
🔍

## Credits

National Institute of Technology (NIT), Warangal
M Naveen has created this Calculator and 500+ more calculators!
NSS College of Engineering (NSSCE), Palakkad
Chandana P Dev has verified this Calculator and 1000+ more calculators!

## Flexural Rigidity when Deflection Due to Prestressing for a doubly Harped Tendon is given Solution

STEP 0: Pre-Calculation Summary
Formula Used
flexural_rigidity = (Part of span length*(3-4*Part of span length^2)*Thrust force*Span length^3)/(24*Deflection)
EI = (a*(3-4*a^2)*Ft*L^3)/(24*𝜕)
This formula uses 4 Variables
Variables Used
Part of span length- Part of span length is described as the part of the beam length
Thrust force - Thrust force acting perpendicular to job piece (Measured in Newton)
Span length - Span length is the end to end distance between any beam or slab. (Measured in Meter)
Deflection - The Deflection is the degree to which a structural element is displaced under a load (due to its deformation). (Measured in Meter)
STEP 1: Convert Input(s) to Base Unit
Part of span length: 1.5 --> No Conversion Required
Thrust force: 10 Newton --> 10 Newton No Conversion Required
Span length: 5 Meter --> 5 Meter No Conversion Required
Deflection: 50 Meter --> 50 Meter No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
EI = (a*(3-4*a^2)*Ft*L^3)/(24*𝜕) --> (1.5*(3-4*1.5^2)*10*5^3)/(24*50)
Evaluating ... ...
EI = -9.375
STEP 3: Convert Result to Output's Unit
-9.375 Newton Meter Square --> No Conversion Required
FINAL ANSWER
-9.375 Newton Meter Square <-- flexural rigidity
(Calculation completed in 00.016 seconds)

## < 10+ Calculations of Deflection and Crack Width Calculators

Deflection Due to Prestressing for a Parabolic Tendon
deflection = (5/384)*((upward thrust*Span length^4)/ (Young's Modulus*Moment of Inertia)) Go
Moment of Inertia(I) when Deflection Due to Prestressing for a Parabolic Tendon is given
moment_of_inertia = (5/384)*((upward thrust*Span length^4)/(Young's Modulus*Deflection)) Go
Length of Span when Deflection Due to Prestressing for a Parabolic Tendon is given
span_length = ((Deflection*384*Young's Modulus*Moment of Inertia)/(5*upward thrust))^(1/4) Go
Young's Modulus when Deflection Due to Prestressing for a Parabolic Tendon is given
youngs_modulus = (5/384)*((upward thrust*Span length^4)/(Deflection*Moment of Inertia)) Go
Length of Span when Deflection Due to Prestressing for a Singly Harped Tendon is given
span_length = ((Deflection*48*Young's Modulus*Moment of Inertia)/Thrust force)^(1/3) Go
Uplift Thrust when Deflection Due to Prestressing for a Parabolic Tendon
upward_thrust = (Deflection*384*Young's Modulus*Moment of Inertia)/(5*Span length^4) Go
Deflection Due to Prestressing for a Singly Harped Tendon
deflection = (Thrust force*Span length^3)/(48*Young's Modulus*Moment of Inertia) Go
Uplift Thrust when Deflection Due to Prestressing for a Singly Harped Tendon is given
thrust_force = (Deflection*48*Young's Modulus*Moment of Inertia)/Span length^3 Go
Flexural Rigidity when Deflection Due to Prestressing for a Parabolic Tendon is given
flexural_rigidity = (5/384)*((upward thrust*Span length^4)/Deflection) Go
Flexural Rigidity when Deflection Due to Prestressing for a Singly Harped Tendon is given
flexural_rigidity = (Thrust force*Span length^3)/(48*Deflection) Go

### Flexural Rigidity when Deflection Due to Prestressing for a doubly Harped Tendon is given Formula

flexural_rigidity = (Part of span length*(3-4*Part of span length^2)*Thrust force*Span length^3)/(24*Deflection)
EI = (a*(3-4*a^2)*Ft*L^3)/(24*𝜕)

## What does deflection Mean?

The Deflection Due to Prestressing for a doubly harped tendon Tendon, deflection of prestressed concrete members is complicated by such factors as the gradual reduction of prestress force due to time-dependent losses, relatively simple procedures.

## How to Calculate Flexural Rigidity when Deflection Due to Prestressing for a doubly Harped Tendon is given?

Flexural Rigidity when Deflection Due to Prestressing for a doubly Harped Tendon is given calculator uses flexural_rigidity = (Part of span length*(3-4*Part of span length^2)*Thrust force*Span length^3)/(24*Deflection) to calculate the flexural rigidity, The Flexural Rigidity when Deflection Due to Prestressing for a doubly Harped Tendon is given is defined as the force couple required to bend a fixed non-rigid structure by one unit of curvature. flexural rigidity and is denoted by EI symbol.

How to calculate Flexural Rigidity when Deflection Due to Prestressing for a doubly Harped Tendon is given using this online calculator? To use this online calculator for Flexural Rigidity when Deflection Due to Prestressing for a doubly Harped Tendon is given, enter Part of span length (a), Thrust force (Ft), Span length (L) and Deflection (𝜕) and hit the calculate button. Here is how the Flexural Rigidity when Deflection Due to Prestressing for a doubly Harped Tendon is given calculation can be explained with given input values -> -9.375 = (1.5*(3-4*1.5^2)*10*5^3)/(24*50).

### FAQ

What is Flexural Rigidity when Deflection Due to Prestressing for a doubly Harped Tendon is given?
The Flexural Rigidity when Deflection Due to Prestressing for a doubly Harped Tendon is given is defined as the force couple required to bend a fixed non-rigid structure by one unit of curvature and is represented as EI = (a*(3-4*a^2)*Ft*L^3)/(24*𝜕) or flexural_rigidity = (Part of span length*(3-4*Part of span length^2)*Thrust force*Span length^3)/(24*Deflection). Part of span length is described as the part of the beam length, Thrust force acting perpendicular to job piece, Span length is the end to end distance between any beam or slab and The Deflection is the degree to which a structural element is displaced under a load (due to its deformation).
How to calculate Flexural Rigidity when Deflection Due to Prestressing for a doubly Harped Tendon is given?
The Flexural Rigidity when Deflection Due to Prestressing for a doubly Harped Tendon is given is defined as the force couple required to bend a fixed non-rigid structure by one unit of curvature is calculated using flexural_rigidity = (Part of span length*(3-4*Part of span length^2)*Thrust force*Span length^3)/(24*Deflection). To calculate Flexural Rigidity when Deflection Due to Prestressing for a doubly Harped Tendon is given, you need Part of span length (a), Thrust force (Ft), Span length (L) and Deflection (𝜕). With our tool, you need to enter the respective value for Part of span length, Thrust force, Span length and Deflection 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 flexural rigidity?
In this formula, flexural rigidity uses Part of span length, Thrust force, Span length and Deflection. We can use 10 other way(s) to calculate the same, which is/are as follows -
• deflection = (5/384)*((upward thrust*Span length^4)/ (Young's Modulus*Moment of Inertia))
• upward_thrust = (Deflection*384*Young's Modulus*Moment of Inertia)/(5*Span length^4)
• flexural_rigidity = (5/384)*((upward thrust*Span length^4)/Deflection)
• span_length = ((Deflection*384*Young's Modulus*Moment of Inertia)/(5*upward thrust))^(1/4)
• youngs_modulus = (5/384)*((upward thrust*Span length^4)/(Deflection*Moment of Inertia))
• moment_of_inertia = (5/384)*((upward thrust*Span length^4)/(Young's Modulus*Deflection))
• deflection = (Thrust force*Span length^3)/(48*Young's Modulus*Moment of Inertia)
• thrust_force = (Deflection*48*Young's Modulus*Moment of Inertia)/Span length^3
• flexural_rigidity = (Thrust force*Span length^3)/(48*Deflection)
• span_length = ((Deflection*48*Young's Modulus*Moment of Inertia)/Thrust force)^(1/3)
Where is the Flexural Rigidity when Deflection Due to Prestressing for a doubly Harped Tendon is given calculator used?
Among many, Flexural Rigidity when Deflection Due to Prestressing for a doubly Harped Tendon is given calculator is widely used in real life applications like {FormulaUses}. Here are few more real life examples -
{FormulaExamplesList} Let Others Know
LinkedIn
Email
WhatsApp
Copied!