Eccentric Point Load for Simply Supported Beam Formula

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Eccentric Point Load For Simply Supported Beam is a type of load applied at a point on a simply supported beam, causing bending and deflection. Check FAQs
ws=3δEILba2b2[g]
ws - Eccentric Point Load For Simply Supported Beam?δ - Static Deflection?E - Young's Modulus?I - Moment of Inertia of Beam?Lb - Beam Length?a - Distance of Load From One End?b - Distance of Load From Other End?[g] - Gravitational acceleration on Earth?

Eccentric Point Load for Simply Supported Beam Example

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Here is how the Eccentric Point Load for Simply Supported Beam equation looks like with Values.

Here is how the Eccentric Point Load for Simply Supported Beam equation looks like with Units.

Here is how the Eccentric Point Load for Simply Supported Beam equation looks like.

0.3034Edit=30.072Edit15Edit6Edit4.8Edit4Edit21.4Edit29.8066
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Eccentric Point Load for Simply Supported Beam Solution

Follow our step by step solution on how to calculate Eccentric Point Load for Simply Supported Beam?

FIRST Step Consider the formula
ws=3δEILba2b2[g]
Next Step Substitute values of Variables
ws=30.072m15N/m6m⁴/m4.8m4m21.4m2[g]
Next Step Substitute values of Constants
ws=30.072m15N/m6m⁴/m4.8m4m21.4m29.8066m/s²
Next Step Prepare to Evaluate
ws=30.0721564.8421.429.8066
Next Step Evaluate
ws=0.30341759969833
LAST Step Rounding Answer
ws=0.3034

Eccentric Point Load for Simply Supported Beam Formula Elements

Variables
Constants
Eccentric Point Load For Simply Supported Beam
Eccentric Point Load For Simply Supported Beam is a type of load applied at a point on a simply supported beam, causing bending and deflection.
Symbol: ws
Measurement: NAUnit: Unitless
Note: Value can be positive or negative.
Static Deflection
Static Deflection is the maximum displacement of a beam under various types of loads and load conditions, affecting its structural integrity and stability.
Symbol: δ
Measurement: LengthUnit: m
Note: Value should be greater than 0.
Young's Modulus
Young's Modulus is a measure of the stiffness of a solid material and is used to predict the amount of deformation under a given load.
Symbol: E
Measurement: Stiffness ConstantUnit: N/m
Note: Value should be greater than 0.
Moment of Inertia of Beam
Moment of Inertia of Beam is a measure of the beam's resistance to bending under various types of loads and load conditions, influencing its structural integrity.
Symbol: I
Measurement: Moment of Inertia per Unit LengthUnit: m⁴/m
Note: Value should be greater than 0.
Beam Length
Beam Length is the horizontal distance between two supports of a beam, used to calculate loads and stresses on various types of beams under different load conditions.
Symbol: Lb
Measurement: LengthUnit: m
Note: Value should be greater than 0.
Distance of Load From One End
Distance of Load From One End is the horizontal distance of the load from one end of the beam, used to calculate beam deflection and stress.
Symbol: a
Measurement: LengthUnit: m
Note: Value should be greater than 0.
Distance of Load From Other End
Distance of Load From Other End is the horizontal distance from the load to the other end of the beam, considering various types of beams and load conditions.
Symbol: b
Measurement: LengthUnit: m
Note: Value should be greater than 0.
Gravitational acceleration on Earth
Gravitational acceleration on Earth means that the velocity of an object in free fall will increase by 9.8 m/s2 every second.
Symbol: [g]
Value: 9.80665 m/s²

Other formulas in Load for Various Types of Beams and Load Conditions category

​Go Value of Load for Fixed Beam with Uniformly Distributed Load
Wf=384δEILb4
​Go Value of Load for Fixed Beam with Central Point Load
wc=192δEILb3

How to Evaluate Eccentric Point Load for Simply Supported Beam?

Eccentric Point Load for Simply Supported Beam evaluator uses Eccentric Point Load For Simply Supported Beam = (3*Static Deflection*Young's Modulus*Moment of Inertia of Beam*Beam Length)/(Distance of Load From One End^2*Distance of Load From Other End^2*[g]) to evaluate the Eccentric Point Load For Simply Supported Beam, Eccentric Point Load for Simply Supported Beam formula is defined as a measure of the load applied at a point on a simply supported beam, which is eccentric to the beam's longitudinal axis, causing bending and deflection of the beam, and is used to calculate the maximum stress and deflection of the beam under various load conditions. Eccentric Point Load For Simply Supported Beam is denoted by ws symbol.

How to evaluate Eccentric Point Load for Simply Supported Beam using this online evaluator? To use this online evaluator for Eccentric Point Load for Simply Supported Beam, enter Static Deflection (δ), Young's Modulus (E), Moment of Inertia of Beam (I), Beam Length (Lb), Distance of Load From One End (a) & Distance of Load From Other End (b) and hit the calculate button.

FAQs on Eccentric Point Load for Simply Supported Beam

What is the formula to find Eccentric Point Load for Simply Supported Beam?
The formula of Eccentric Point Load for Simply Supported Beam is expressed as Eccentric Point Load For Simply Supported Beam = (3*Static Deflection*Young's Modulus*Moment of Inertia of Beam*Beam Length)/(Distance of Load From One End^2*Distance of Load From Other End^2*[g]). Here is an example- 0.303418 = (3*0.072*15*6*4.8)/(4^2*1.4^2*[g]).
How to calculate Eccentric Point Load for Simply Supported Beam?
With Static Deflection (δ), Young's Modulus (E), Moment of Inertia of Beam (I), Beam Length (Lb), Distance of Load From One End (a) & Distance of Load From Other End (b) we can find Eccentric Point Load for Simply Supported Beam using the formula - Eccentric Point Load For Simply Supported Beam = (3*Static Deflection*Young's Modulus*Moment of Inertia of Beam*Beam Length)/(Distance of Load From One End^2*Distance of Load From Other End^2*[g]). This formula also uses Gravitational acceleration on Earth constant(s).
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