Question 14 Marks
Read the passage given below and answer the following questions from 1 to 3. Bernoulli's Theorem It states that for the streamline flow of an ideal liquid through a tube, the total energy (the sum of pressure energy, the potential energy and kinetic energy) per unit volume remains constant at every cross-section throughout the tube.$\text{P}+\text{pgh}+\frac{1}{2}\text{pv}^2$ = constant
or $\frac{\text{P}}{\text{pg}}+\text{h}+\frac{1}{2}\frac{\text{v}^2}{\text{g}}$ = another constant Here, $\frac{\text{P}}{\text{pg}}$ = pressure head; h = potential head and $\frac{1}{2}\frac{\text{v}^2}{\text{g}}$ velocity head. If the liquid is flowing through a horizontal tube, then h is constant, then according to Bernoulli’s theorem,$\frac{\text{P}}{\text{pg}}+\frac{1}{2}\frac{\text{v}^2}{\text{g}}$ constant
Bernoulli’s theorem is based on law of conser - vation of energy.
or $\frac{\text{P}}{\text{pg}}+\text{h}+\frac{1}{2}\frac{\text{v}^2}{\text{g}}$ = another constant Here, $\frac{\text{P}}{\text{pg}}$ = pressure head; h = potential head and $\frac{1}{2}\frac{\text{v}^2}{\text{g}}$ velocity head. If the liquid is flowing through a horizontal tube, then h is constant, then according to Bernoulli’s theorem,$\frac{\text{P}}{\text{pg}}+\frac{1}{2}\frac{\text{v}^2}{\text{g}}$ constant
Bernoulli’s theorem is based on law of conser - vation of energy.
- Bernoulli’s equation for steady, non-viscous, incompressible flow expresses the:
- Conservation of linear momentum
- Conservation of angular momentum
- Conservation of energy
- Conservation of mass
- Applications of Bernoulli’s theorem can be seen in:
- Dynamic lift of aeroplane
- Hydraulic press
- Helicopter
- None of these
- A tank filled with fresh water has a hole in its bottom and water is flowing out of it. If the size of the hole is increased, then:
- The volume of water flowing out per second will decrease.
- The velocity of outflow of water remains unchanged.
- The volume of water flowing out per second remains zero.
- Both (b) and (c)
Answer
Bernoullis equation for steady, non-viscous, in compressible flow express the conservation of energy.
The shape of the aeroplane wings is such that when it moves forward, the air molecules at the top of the wings have a greater velocity (relative to the wings) compared to the air molecules at the bottom.
Therefore in accordance with Bernoulli's principle, the pressure at the top of the wings is less than that at the bottom.
This results in a dynamic lift of the wings which balances the weight of the plane.
The velocity of outflow of water remains unchanged because it depends upon the height of water level and is independent of the size of the hole.
The volume depends directly on the size of the hole.
View full question & answer→- (c) Conservation of energy
Bernoullis equation for steady, non-viscous, in compressible flow express the conservation of energy.
- (a) Dynamic lift of aeroplane
The shape of the aeroplane wings is such that when it moves forward, the air molecules at the top of the wings have a greater velocity (relative to the wings) compared to the air molecules at the bottom.
Therefore in accordance with Bernoulli's principle, the pressure at the top of the wings is less than that at the bottom.
This results in a dynamic lift of the wings which balances the weight of the plane.
- (b) The velocity of outflow of water remains unchanged.
The velocity of outflow of water remains unchanged because it depends upon the height of water level and is independent of the size of the hole.
The volume depends directly on the size of the hole.