When a container open to atmmosphere , obtain the velocity of liquid coming out of the narrow hole from the wall of container by using Bernoulli's equation and obtain Torricelli's law
When a container open to atmmosphere , obtain the velocity of liquid coming out of the narrow hole from the wall of container by using Bernoulli's equation and obtain Torricelli's law
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Torricelli.s discovered that speed of efflux from an open tank is given by a formula identical to that of a freely falling body .
Consider a tank containing a liquid of density `rho` with a small hole in its side at a height `y_(1)` from the bottom . the air above the liquid , whose surface is at height `y_(2)` is at pressure P.
The velocities `v_(1)andv_(2)` are at point 1 and 2 respectively.
Using equation of continuity for points 1 and 2,
`A_(1)v_(1)=A_(2)v_(2)`
`v_(2)=(A_(1)v_(1))/(A_(2))` ..... (1)
`A_(2)` is the cross sectional area of the tank and
`A_(1)` is the cross sectional area of the hole
`A_(2)gtgtA_(1)` hence
`v_(2)ltltv_(1)thereforev_(2)=0`.
Using Bernoulli.s equation at 1 and 2
`P_(1)+(1)/(2)rhov_(1)^(2)+rhogy_(1)=P_(2)+(1)/(2)rhov_(2)^(2)+rhogy_(2)`
Here `P_(1)=` atmospheric pressure `P_(a)`
`P_(2)=P`
`v_(2)=0`
`P_(a)+(1)/(2)rhov_(1)^(2)+rhogy_(1)=P+rhogy_(2)`
`therefore(1)/(2)rhov_(1)^(2)=(P-P_(a))+rhog(y_(2)-y_(1))`
Taking h as the difference in height `=y_(2)-y_(1)(1)/(2)rhov_(1)^(2)=(P-P_(a))+rhogh`
`v_(1)=sqrt(2gh+(2(P-P_(a)))/(rho))` .... (2)
Special Cases : `(1)PgtgtP_(a),2gh` is neglecting with the value of `(P-P_(a))`.
`thereforev_(1)=sqrt((2(P-P_(a)))/(rho))` ....(3)
Hence , the speed of efflux determined only by the pressure of container . Such a situation occurs in rocket propulsion where efflux means coming out liquid.
(2) If the tank is open to atmosphere , then
`P=P_(a)` and equation (2) becomes as below.
`v_(1)=sqrt(2gh)` .... (4)
This is the speed of a freely falling body . This equation is known as Torricelli.s law.
Consider a tank containing a liquid of density `rho` with a small hole in its side at a height `y_(1)` from the bottom . the air above the liquid , whose surface is at height `y_(2)` is at pressure P.
The velocities `v_(1)andv_(2)` are at point 1 and 2 respectively.
Using equation of continuity for points 1 and 2,
`A_(1)v_(1)=A_(2)v_(2)`
`v_(2)=(A_(1)v_(1))/(A_(2))` ..... (1)
`A_(2)` is the cross sectional area of the tank and
`A_(1)` is the cross sectional area of the hole
`A_(2)gtgtA_(1)` hence
`v_(2)ltltv_(1)thereforev_(2)=0`.
Using Bernoulli.s equation at 1 and 2
`P_(1)+(1)/(2)rhov_(1)^(2)+rhogy_(1)=P_(2)+(1)/(2)rhov_(2)^(2)+rhogy_(2)`
Here `P_(1)=` atmospheric pressure `P_(a)`
`P_(2)=P`
`v_(2)=0`
`P_(a)+(1)/(2)rhov_(1)^(2)+rhogy_(1)=P+rhogy_(2)`
`therefore(1)/(2)rhov_(1)^(2)=(P-P_(a))+rhog(y_(2)-y_(1))`
Taking h as the difference in height `=y_(2)-y_(1)(1)/(2)rhov_(1)^(2)=(P-P_(a))+rhogh`
`v_(1)=sqrt(2gh+(2(P-P_(a)))/(rho))` .... (2)
Special Cases : `(1)PgtgtP_(a),2gh` is neglecting with the value of `(P-P_(a))`.
`thereforev_(1)=sqrt((2(P-P_(a)))/(rho))` ....(3)
Hence , the speed of efflux determined only by the pressure of container . Such a situation occurs in rocket propulsion where efflux means coming out liquid.
(2) If the tank is open to atmosphere , then
`P=P_(a)` and equation (2) becomes as below.
`v_(1)=sqrt(2gh)` .... (4)
This is the speed of a freely falling body . This equation is known as Torricelli.s law.
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