Deflection for Axial Compression and Bending Solution

STEP 0: Pre-Calculation Summary
Formula Used
Deflection of Beam = Deflection for Transverse Loading Alone/(1-(Axial Load/Critical Buckling Load))
δ = d0/(1-(P/Pc))
This formula uses 4 Variables
Variables Used
Deflection of Beam - (Measured in Meter) - Deflection of Beam Deflection is the movement of a beam or node from its original position. It happens due to the forces and loads being applied to the body.
Deflection for Transverse Loading Alone - (Measured in Meter) - Deflection for Transverse Loading Alone is defined as the deflections caused in the beam due to the transverse load alone.
Axial Load - (Measured in Newton) - Axial Load is a force applied on a structure directly along an axis of the structure.
Critical Buckling Load - (Measured in Newton) - Critical Buckling Load is the maximum load that a column can take before deformation.
STEP 1: Convert Input(s) to Base Unit
Deflection for Transverse Loading Alone: 4 Millimeter --> 0.004 Meter (Check conversion ​here)
Axial Load: 2000 Newton --> 2000 Newton No Conversion Required
Critical Buckling Load: 12000 Newton --> 12000 Newton No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
δ = d0/(1-(P/Pc)) --> 0.004/(1-(2000/12000))
Evaluating ... ...
δ = 0.0048
STEP 3: Convert Result to Output's Unit
0.0048 Meter -->4.8 Millimeter (Check conversion ​here)
FINAL ANSWER
4.8 Millimeter <-- Deflection of Beam
(Calculation completed in 00.004 seconds)

Credits

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Created by Kethavath Srinath
Osmania University (OU), Hyderabad
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Verified by Rudrani Tidke
Cummins College of Engineering for Women (CCEW), Pune
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Combined Axial and Bending Loads Calculators

Maximum Bending Moment given Maximum Stress for Short Beams
​ LaTeX ​ Go Maximum Bending Moment = ((Maximum Stress-(Axial Load/Cross Sectional Area))*Area Moment of Inertia)/Distance from Neutral Axis
Cross-Sectional Area given Maximum Stress for Short Beams
​ LaTeX ​ Go Cross Sectional Area = Axial Load/(Maximum Stress-((Maximum Bending Moment*Distance from Neutral Axis)/Area Moment of Inertia))
Axial Load given Maximum Stress for Short Beams
​ LaTeX ​ Go Axial Load = Cross Sectional Area*(Maximum Stress-((Maximum Bending Moment*Distance from Neutral Axis)/Area Moment of Inertia))
Maximum Stress for Short Beams
​ LaTeX ​ Go Maximum Stress = (Axial Load/Cross Sectional Area)+((Maximum Bending Moment*Distance from Neutral Axis)/Area Moment of Inertia)

Deflection for Axial Compression and Bending Formula

​LaTeX ​Go
Deflection of Beam = Deflection for Transverse Loading Alone/(1-(Axial Load/Critical Buckling Load))
δ = d0/(1-(P/Pc))

Define Deflection

Deflection is the degree to which a structural element is displaced under a load (due to its deformation). It may refer to an angle or a distance. The deflection distance of a member under a load can be calculated by integrating the function that mathematically describes the slope of the deflected shape of the member under that load.

How to Calculate Deflection for Axial Compression and Bending?

Deflection for Axial Compression and Bending calculator uses Deflection of Beam = Deflection for Transverse Loading Alone/(1-(Axial Load/Critical Buckling Load)) to calculate the Deflection of Beam, The Deflection for Axial Compression and Bending formula is defined as the degree to which an element of structure changes shape when a load is applied. Deflection of Beam is denoted by δ symbol.

How to calculate Deflection for Axial Compression and Bending using this online calculator? To use this online calculator for Deflection for Axial Compression and Bending, enter Deflection for Transverse Loading Alone (d0), Axial Load (P) & Critical Buckling Load (Pc) and hit the calculate button. Here is how the Deflection for Axial Compression and Bending calculation can be explained with given input values -> 0.0048 = 0.004/(1-(2000/12000)).

FAQ

What is Deflection for Axial Compression and Bending?
The Deflection for Axial Compression and Bending formula is defined as the degree to which an element of structure changes shape when a load is applied and is represented as δ = d0/(1-(P/Pc)) or Deflection of Beam = Deflection for Transverse Loading Alone/(1-(Axial Load/Critical Buckling Load)). Deflection for Transverse Loading Alone is defined as the deflections caused in the beam due to the transverse load alone, Axial Load is a force applied on a structure directly along an axis of the structure & Critical Buckling Load is the maximum load that a column can take before deformation.
How to calculate Deflection for Axial Compression and Bending?
The Deflection for Axial Compression and Bending formula is defined as the degree to which an element of structure changes shape when a load is applied is calculated using Deflection of Beam = Deflection for Transverse Loading Alone/(1-(Axial Load/Critical Buckling Load)). To calculate Deflection for Axial Compression and Bending, you need Deflection for Transverse Loading Alone (d0), Axial Load (P) & Critical Buckling Load (Pc). With our tool, you need to enter the respective value for Deflection for Transverse Loading Alone, Axial Load & Critical Buckling Load and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.
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