when the load is applied in the beam then deflection takes place.
the nature of the deflection depends on the support provided on it
when the load applied on the beam it transfer the load from upper side to bottom side and pass through the column.
the beam gets bend if the load is more then the resisting force of the beam and if the resisting force is more then the load it doesn't bends.
it will depend upon the load and moment applied on the beam.
Deflection of simply supported beam is given by P*l^3/(48E) Where P= point load at centre of beam l= length of beam E= Modules of elasticity
A uniformly distributed load is one which the load is spread evenly across the full length of the beam (i.e. there is equal loading per unit length of the beam).
Deflection of beam depends upon load and length of beam. Larger the beam, larger will be it's selfweight
It is a load applied slowly rather than quickly or suddenly. If applied quickly, the problem becomes one of dynamics, or impulse loading, but if applied slowly (gradual) it is a statics problem
The beam will deflect in the direction of the load This is Hooke's law, which states that load is proportional to deflection
the beam gets bend if the load is more then the resisting force of the beam and if the resisting force is more then the load it doesn't bends.
it will depend upon the load and moment applied on the beam.
bottom
It depends on the stress/load applied to a beam, but a general rule is to provide a lap where the stress is the least. In a simply supported beam with a uniformly distributed load the best place to position laps would be away from the centre of the beam.
It all depends on the dimensions of the steel beam
You compress it Well, it ALL depends on how hard you push down on the spring.
defination of suddenly applied load
Stiffness is defined as the ratio of load per unit deformation.
defination of suddenly applied load
defination of suddenly applied load
The moment of a beam is twice that for central load vs uniform load for a simple support beam; hence it needs twice the section modulus for sizing; for fixed ends the moment is 50% higher for central load vs uniform load