Find out the deflection - vertical, Mechanical Engineering

Assignment Help:

Find out the deflection:

Find out the deflection (vertical) at a distance 'a' from the tip in Example

Solution

As in this case there is no load at the point where the deflection is required, we introduce a fictitious load Q as illustrated in Figure.

260_Find out the deflection.png

Figure

 Then,

M = - Px  and    ∂M /∂Q  = 0   for   0 ≤ x ≤ a

and

M = - Px - Q ( x - a)   and   ∂M/∂Q    = - ( x - a)   for   a ≤ x ≤ L

2144_Find out the deflection1.png


Related Discussions:- Find out the deflection - vertical

Calculate composition and microstructure, It is desired to produce an iron-...

It is desired to produce an iron-carbon alloy that has a minimum hardness of 200 HB and a minimum ductility of 35%RA. Is such an alloy possible? If so, what will be its composition

Evaluate the work done by the gas during the expansion, (a) What do you und...

(a) What do you understand by the following : (i) Open System (ii) Closed System (iii) Concept of ‘Work' (b) 0.014 m 3 gas at a pressure of 2070 KPa expends to a pressure of

Takt time for sand blasting, Takt Time for sand blasting:            ...

Takt Time for sand blasting:             Tatk time is crucial in manufacturing process. It determines the speed of production to produce a product. Time is money toward prod

Internal combustion engine - thermodynamics, Internal combustion engine - T...

Internal combustion engine - Thermodynamics: Internal combustion engine is popularly known as I.C. engine, is heat engine that converts the heat energy released by the combust

Torsion, series shaft and parallel shaft

series shaft and parallel shaft

Describe that energy is a point function, (a) Describe that Energy is a poi...

(a) Describe that Energy is a point function and a property of the system. (b) What is the essence of 1 st law of thermodynamics ? Write down expression for the first law appli

Single-engine general aviation aircraft, The wing of a light, single-engine...

The wing of a light, single-engine general aviation aircraft has an area of 15.8 m 2 and a span of 9.6 m. The airfoil of the wing is NACA 65-415, which has a lift slope of 0.1033

#strength of materials., derivation of elongation of bar due to its self we...

derivation of elongation of bar due to its self weight

Write Your Message!

Captcha
Free Assignment Quote

Assured A++ Grade

Get guaranteed satisfaction & time on delivery in every assignment order you paid with us! We ensure premium quality solution document along with free turntin report!

All rights reserved! Copyrights ©2019-2020 ExpertsMind IT Educational Pvt Ltd