Physics Bernoulis Theorem Project CBSE Class 12

CHOITHRAM SCHOOL (MANIK BAGH)

PHYSICS INVESTIGATORY PROJECT BERNOULLI’S THEOREM

SESSION: 2016-2017

Submitted to-

Submitted by-

Mrs.Kalpana Tiwari

Pradeep Singh Rathour

CERTIFICATE

This is to certify that PRADEEP SINGH RATHOUR is a student of

class XI C has

successfully completed the research on the below mentioned project under the guidance of

Mrs. Kalpana Tiwari (subject teacher)

during year 2016-17 in partial fulfillment of chemistry practical examination . ofcentral board of secondary education (CBSE)

PRINCIPAL MR. RAJESH AWASTHI

SUBJECT TEACHER

Mrs. Kalpana Tiwari

Page 2 of 21

DECLARATION I hereby declare that the project work entitled

“BERNAULLI’S

PRINCIPLE”

submitted to the “CHOITHRAM SCHOOL “, is a record of original work done by me except of the experiments, which are duly acknowledged , under the guidance of my subject teacher “Mrs. KALPANA TIWARI” and “Mr. Gaurav Tiwari”.

Page 3 of 21

ACKNOWLEDGMENT I would like to express my special thanks to our school ‘CHOITHRAM SCHOOL’, principal sir Mr. ‘RAJESH AWASTHI’, to the management team of our school who gave me the golden opportunity to do this wonderful project on the topic BERNAULLI’S PRINCIPLE, which also helped me in doing a lot of research and I came to know about so many new things. Secondly I would also like to thank my parents and friends who helped me a lot in finishing this project within the limited time.

Page 4 of 21

INDEX 1. 2. 3. 4. 5. 6. 7. 8. 9. 10.

PRESSURE Pascal’s Law Hydraulics Continuity Equation Bernoulli’s Equation Derivation of Bernoulli’s Equation Venturi Tube Atomizer Torricelli and his Orifice Derivation of Torricelli’s Equation

11. Streamlines 12. Aerodynamic Lift 13. Misconceptions of Lift 14. Conclusion 15. Bibliography Page 5 of 21

PRESSURE 1. Pressure is defined as force per unit area. 2. Standard unit is Pascal, which is N/m2 3. For liquid pressure, the medium is considered as a continuous distribution of matter. 4. For gas pressure, it is calculated as the average pressure of molecular collisions on the container. 5. Pressure acts perpendicular on the surface. 6. Pressure is a scalar quantity – pressure has no particular direction (i.e. acts in every direction).

Page 6 of 21

Pascal’s Law Pf = P0 + ρgh 1. “When there is an increase in pressure at any point in a confined fluid, there is an equal increase at every point in the container.” 2. In a fluid, all points at the same depth must be at the same pressure. 3. Consider a fluid in equilibrium.

Page 7 of 21

Hydraulics

You have to push down the piston on the left far down to achieve some change in the height of the piston on the right.

1. Pressure is equal at the bottom of both containers (because it’s the same depth!) 2. P = F2/A2 = F1/A1 and since A1 < A2, F2 > F1 3. There is a magnification of force, just like a lever, but work stays the same! (conservation of energy). W = F1* D1 = F2 * D2 ∴ D1 > D2

Page 8 of 21

Continuity Equation

1.

A1v1 = A2v2

2.

“What comes in comes out.”

3.

Av= V/s (volume flow rate) = constant Page 9 of 21

Bernoulli’s Equation P+1/2ρv*v+ρgh=constant Where p is the pressure, ρ is the density, v is the velocity, h is elevation, and g is gravitational acceleration

Page 10 of 21

Derivation of Bernoulli’s Equation

 

Restrictions Incompressible



Non-viscous fluid (i.e. no friction)



Following a streamline motion (no

turbulence) 

Constant density

*There exists an extended form of equation that takes friction and compressibility into account, but that is too complicated for our level of study.

Page 11 of 21

Etotal = 1/2mv2 + mgh W = F/A*A*d = PV

 Consider the change in total energy of the fluid as it moves from the inlet to the outlet.

Δ Etotal = Wdone on fluid - Wdone by fluid Δ Etotal = (1/2mv22 + mgh1) – (1/2mv12 + mgh2) Wdone on fluid - Wdone by fluid = (1/2mv22 + mgh1) – (1/2mv12 + mgh2) P2V2 - P1V1 = (1/2mv22 + mgh1) – (1/2mv12 + mgh2) P2 – P1 = (1/2ρ v12 + ρ gh1) – (1/2ρ v12 + ρ gh1) Page 12 of 21

Venturi Tube

1. A2 < A1 ; V2 > V1 2. According to Bernoulli’s Law, pressure at A2 is lower. 3. Choked flow: Because pressure cannot be negative, total flow rate will be limited. This is useful in controlling fluid velocity. P2 + 1/2ρ v12 = P1 + 1/2ρ v12 ΔP = ρ/2*(v22 – v12)

;

Page 13 of 21

Atomizer

• This is an atomizer, which uses the Venturi effect to spray liquid. • When the air stream from the hose flows over the straw, the resulting low pressure on the top lifts up the fluid. Page 14 of 21

Torricelli and his Orifice  In 1843, Evangelista Torricelli proved that the flow of liquid through an opening is proportional to the square root of the height of the opening.  Q = A*√(2g(h1-h2)) where Q is flow rate, A is area, h is height Depending on the contour and shape of the opening, different discharge coefficients can be applied to the equation (of course we assume simpler situation here

Page 15 of 21

Derivation of Torricelli’s Equation 1. We use the Bernoulli Equation: 2. In the original diagram A1 [top] is much larger than A2 [the opening]. Since A1V1 = A2V2 and A1 >> A2, V1 ≈ 0 3. Since both the top and the opening are open to atmospheric pressure, P1 = P2 = 0 (in gauge pressure). The equation simplifies down to: ρgh1 = 1/2 ρv22 + ρgh2 /2 ρv22 = pg(h1-h2)

1

V22 = 2g(h1-h2) ∴ V2 = √(2g(h1-h2)) Q = Av2 = A √(2g(h1-h2)) Page 16 of 21

Streamlines 1

A streamline is a path traced out by a massless particle as it moves with the flow. 2. Velocity is zero at the surface. 1. As you move away from the surface, the velocity uniformly approaches the free stream value (fluid molecules nearby the surface are dragged due to viscosity). 2. The layer at which the velocity reaches the free stream value is called boundary layer. It does not necessarily match the shape of the object – boundary layer can be detached, creating turbulence (wing stall in aerodynamic terms).

Page 17 of 21

Aerodynamic Lift 1. Lift is the fort that keeps an aircraft in the air. 2. In Bernoulli-an view, lift is produced by the different of pressure (faster velocity on the top, slower velocity in the bottom) 3. In Newtonian view, lift is the reaction force that results from the downward deflection of the air. 3. 4.

Both views are correct, but the current argument arises from the misapplication of either view. The most accurate explanation would take into account the simultaneous conservation of mass, momentum, and energy of a fluid, but that involves multivariable calculus.

Page 18 of 21

Misconceptions of Lift 1. In many popular literature, encyclopedia, and even textbooks, Bernoulli’s Law is used incorrectly to explain the aerodynamic lift. #1: Equal transit time - The air on the upper side of the wing travels faster because it has to travel a longer path and must “catch up” with the air on the lower side. The error lies in the specification of velocity. Air is not forced to “catch up” with the downside air. Also, this theory predicts slower velocity than in reality.

Page 19 of 21

Conclusion Bernoulli's law states that if a non-viscous fluid is flowing along a pipe of varying cross section, then the pressure is lower at constrictions where the velocity is higher, and the pressure is higher where the pipe opens out and the fluid stagnate. Many people find this situation paradoxical when they first encounter it (higher velocity, lower pressure). Venturimeter, atomiser and filter pump Bernoulli’s principle is used in venturimeter to find the rate of flow of a liquid. It is used in a carburettor to mix air and petrol vapour in an internal combustion engine. Bernoulli’s principle is used in an atomiser and filter pump. Wings of Aeroplane Wings of an aeroplane are made tapering. The upper surface is made convex and the lower surface is made concave. Due to this shape of the wing, the air currents at the top have a large velocity than at the bottom. Consequently the pressure above the surface of the wing is less as compared to the lower surface of the wing. This difference of pressure is helpful in giving a vertical lift to the plane.

Page 20 of 21

BIBLIOGRAPHY 1. Help from Internet  www.sceincefare.com  www.mycbsegide.com 2. Help from books  Refrenced from H.C.Verma  Refrenced from physics NCERT 3. Help from teachers

Page 21 of 21