CRITICAL VELOCITY
Critical velocity is the velocity of liquid below up to which its flow is steady and above which its flow becomes turbulent.
When the velocity of the liquid flowing through a pipe is small, the flow is steady. As velocity is increased, a stage is reached when experiments show that for cylindrical pipes critical velocity is given by
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= Radius of pipe
= Density of the liquid
Derivation of expression for critical velocity
We can derive the formula for critical velocity by dimensional analysis.
The critical velocity vc of a liquid flowing through a pipe depends upon
  1. Coefficient of viscosity of a liquid O19sNspRUOyjUdZ25VP9RwbPMzV6y6Je VVqtzwTBAYQfZnSikmt4QwPA D8kgmdbiuEw38xbkzB5tSzquFXyxDfImESUENxDrGBV0aOpiv9wKbnHLYyYqZHRNCjmNQEWyK93HQ
  2. Density of the liquid BdsZzDzUC0 QTzvFiGV6UqT4l6AMygt0ZBwvudUGnGdhwf1RdCjXjCYbBsniQKv7KVvVrOuOtYW KlFU1rpnt9MgUAg4efbdAtWetXiNCCWWvjEvGTJVwxSO5aYYFJ4eq39qwI
(iii) Radius of the
pipe
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8t3jko5XXqqXn4ai R OavDozn2rkVmQOBqZRq02ofgl3gL3aXFktAiMA7H ZAfO983h4RUfDyPY 50L XIdDflcC914bhHCrDmn2Vl32kb61tkVgbopWak27VoFRi6SOnOpSCQ IIaELh FRYS4Nu3L3xbgoulyVGYm4NkC X RYHYdireAgXrJQV17TOuIHJYn4kDRt3zvKdH2rpu2ubRSEp5fSUwlDQ67WKxDSGUBz W3rTFj5P LXjJH0DsKYwbneI0hjhSpggELgFhJyyEp07eN6mslLatUmREUrnef7Sso RQ2fzOT488i6IpvFUPry1FqSe8sBEqNrxqyitP9pVRcnJCoLDga4 NSmL2tM6wJIaaAVfg5o8BkJayn0Mrj2cCKXYSu 5EsmfgvHY
OHnO0rZTHdxXLvvUfpZeSN46dRJI2lugrObRiVr3aKUZSUN5YCoHn0vna Sm6IMWBStkFtwvlWHAjr8CPk6Rpd1LiZLSNnKmzBna9NIFJB 5klLyLZ6xumFQtF43dIUm OSznM
Equating the powers of M, L and T
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By experiment the value of k = 1100
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EQUATION OF CONTINUITY
(MASS FLOW RATE)
Consider the flowing of the fluid on the pipe PQ as shown on the figure below
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Let
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If YA5yyp1KQ8 RrqQ8F1o7LwdOFoiQ1L56pSWAOlgyzW Q12pOVRIc6HiJLFi V0f0Gy 3tAsQ9DX 13FjdgJjvRoh LmICBVNK JwZaTVRlIjJbYgqSE2Mrk0zK1VxdmzgcLgqUare densities of fluid at P and Q
Mass flow rate
Is the mass of liquid (fluid) flowing through a tube per second.
Then, the rate of mass of fluid leaving at P and Q at the time interval 4K0Uo1iWnNa1IzEWGZF928ojiqk1PPX8qGpSXY5qXDXV3KUohrbeLOxS7rxc22ym8QsDBTGHSx3vo2hxDKYkpU1Mqwgb5PZyQsHMGSTb Kaqv E0fsg5RdCwwDiJQPc5gGLtGa0 be
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SI unit of mass flow rate is kg/s
Applying the law of conservation of mass
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This is the equation of continuity for the compressible fluid flow.
If the liquid is incompressible, the density of liquid P and Q will be equal.
Flow is steady. No liquid can cross the side, so the mass of liquid passing through section P is equal to the mass of liquid passing through section Q in one second.
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Equation of continuity
States that “the mass of a liquid flowing through a pipe of varying cross – section is constant when density of the liquid does not change”.
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AV = Constant.
ENERGY OF A LIQUID
A moving liquid can possess the following types of energies
  1. K.E. due to its position
  2. P.E. due to its position
  3. Pressure energy due to pressure of the liquid
  4. K.E of a liquid
(i) K.E of a liquid
Is the energy possessed by the liquid due to its motion
 0Qz5yKefxO2FlIGt7F MSxq2LxvtGQexrDZnFHlK8XrGzty0GzYzBa9daP5cSDPZyeDWtWlARSCUur8sCHDhxrwaqM2nVrymc JWlqIhhR03ewt0v SUp0THVy CUkDHfzEMMI
M – Mass liquid
V – Velocity of a liquid flow
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(ii) P.E of a liquid
Is the energy possessed by the liquid due to its position
P.E of liquid of mass m at a height h is given by
P.E = 1JZNsa RewyjHrcfIqkVjKac16a1i6A7DUFFdljdmk9kw5yflCPJN8Ai2Jmc5nHG8ptQgRpOxxQNQQk5ozsCKteHhDVqaINWwVveWmU EldqoIghD7KnyhxenHrVC9dfzT9V T4
*P.E per unit mass = 1JZNsa RewyjHrcfIqkVjKac16a1i6A7DUFFdljdmk9kw5yflCPJN8Ai2Jmc5nHG8ptQgRpOxxQNQQk5ozsCKteHhDVqaINWwVveWmU EldqoIghD7KnyhxenHrVC9dfzT9V T4 m=1
AOFw51ysBNEo0H4hnITNmpxR9vjIjKKPp3oz584QILbHzM2T4LHR3Vs HtdtALhdNHYm9Ty3vJG 5I6UV96RF ZOUi2ixIAPx2gX0b4J5hVxbvNmlzIYh9j8XMLK8b8DeAdhvwP.E per unit mass =
4hKk3SlywRveSdGwOxeJ032pRjiRYm4kLkmTT1c7NnCjCxvAp3laOsD0h3K7OCENXKt 93bavVixH3rlsUk8lRTun5TPPKCZnLb6fCJBdpaL9SzuAG TZCK7e7DNloF4C46dgaAImage?w=241&h=152&rev=1&ac=1&parent=1LROdijXKcU8Ys2KKp6YZtwhvOKDJrPcw
In figure below, is a wide tank containing a liquid
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At its bottom there is a side tube fitted with a frictionless piston of area of cross section A.
Work done to move the piston through a small distance X
W = F.X
But,
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P – Pressure on the piston
W = PAX
Mass of liquid pushed
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M = KF7q 3poUNE9qBqo17nPQBAKu60ZBVUO4ar56k8V4ymPlWIqKtgi TbRE1MLc KBlWP9xyALACjQot NhMlerXjpRyN6 R6XD8xr9hf1osv37F2PnN7FNBtNAc J6Ih59NNrzLk
But
V = AX
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This work done is stored in as pressure energy of a column of liquid
Pressure energy = PAX
* Pressure energy per unit mass = Zok2sorVc9mxJiemmTvBq6S01IO4PMu0oIB0xTdlvv2PLDCCCkG7T8OoMSBYiBWY7JXJJalxOZJA4IgpLPCKft8qtXxpIHwQvv LDZp9rPvGcrndHIwuS9z3hbRSL9BmuA1lLo
KF N32Vrj3P6qHkgy6ZgNNo Qx6121t1TF KRfzokfsx0k2T0zOVeeuI29HTJTTIXzzNDhSEuSBX9e3WatUBlU9cg6Pur RXO IZNolkZehIQAFK9hOK5Q6SqvUpTCE4dpF FOw
*Pressure energy per unit volume = 3skiMxq29S9gXxQhflBDuFiOiEE0SMiiNPdTieU93Kwnrz JkBOLmZNXD8Onpgol6ArAXH3UldmTUXd7T XeTUE5KojqQx31HhXgOT53rdDRKG6n9WuR9hi3MaTp 32aRzBHfJ8
Pressure energy per unit volume = P
Pressure energy of a volume V of a liquid is given by = PV
Total energy of moving liquid
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Total energy per unit volume
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Total energy per unit mass
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But
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BERNOULLI’S THEOREM
States that “for steady flow of an ideal liquid, the total energy per unit volume remains constant throughout the flow”.
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P – Pressure within the fluid
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V – Velocity of the fluid
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Bernoulli’s theorem is simply a statement of law of conservation of energy applied to a liquid.
The importance of this theorem lies in the fact it can be used to determine the variation of pressure in liquids as a function of velocity of the liquid and the elevation of the pipe through which the liquid is flowing.
PROOF OF BERNOULLI’S THEOREM
Consider an incompressible, non-viscous fluid flow and steadily through a pipe of variable cross – section. Consider two sections A and Q.
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J3RgcqF6QepAy Mb0q4pSxIMW7bG6mfdWicktY1fsZGFP2plhU2S4DfDDVQsSsuDQtkY8mYGE0JnDYy8641 GqruI8QMImeeB6VNjQk Nxj0dJaDp1I6gLWwLsZkpxTz0G9J3UI – The cross – sectional areas at P and Q
557vjUhbG2GlUhns1n FZXpeIpTZ48KIqSYr4JfxHGzAqTAoMZTstlk SPtGF4jSAqF1QNKLOWmDE1L S3NVL6afGty 1zcHTKXQ M4VxzVjfZE00FVGVD1UA34AuIXCP4Py1KQ – Fluid velocity at P and Q
QvcNZ 3wptu2cNnRvqKFV8oDwwiCNg8w9jYmw2w0BJgHU2duklZ0s0GrayIYXBks WCqMb2X5DOFlVE6fF8EVAI62TMr7XOhvlTXKMACdaAodiw9JuwEL5pIUQWT HluHRn98lw – Fluid pressure at P and Q
46XpWCzxLSn X S Els F8r4eFGsngb5HEmQTJgQuLsxVnpDi6Z1c8pRGkLpEdPt WDaUVTtqL8UxKdQawsGuXcGl7chBVj8agBB 2X TP9IrJxS1YmhO7FhWx5VzyHcx9YdunY – Mean heights above ground level at P and Q respectively
The force acting on the liquid layer at P is
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Under this force in time 4K0Uo1iWnNa1IzEWGZF928ojiqk1PPX8qGpSXY5qXDXV3KUohrbeLOxS7rxc22ym8QsDBTGHSx3vo2hxDKYkpU1Mqwgb5PZyQsHMGSTb Kaqv E0fsg5RdCwwDiJQPc5gGLtGa0 the layer moves through a distance
= FdGNF FDL Ksxacy7LXCmZE5y6Bq6EiKg7dXWWTLFbJjryk6f8fyTUqISMYxZ9ej H6Snzx F4c7MfL7WWTIa0kQu VlnHD9t Fg0stDDZxWvvFAT RialFSqXfB1QxXmF9DNew
Work done on the fluid due to the force
= T5IjC6JLILlxpODvWUb7SspKvBZY4COMk34RgOkV8rLHBtc1RrHhpG5zmcVZj8DsGx5fTcXu4fmufNXx1vuzqBjjxH90qg4Oo738yyMyuNR6h7HZjG YgX5nkpc3WQIBzFYpKu0
When the liquid moves from P to 2xIQo0jp5u328wJIncpkueRdGeSEEzs7RHnOxErNJ502xU2dOBHtIYIq1UOX4yYWog0qzDrp7h9jtC4G8C7DRJL7 A2z96MLTbRoXDki9SLDr V6NsvmxCcf9cK3V Pm9C2hCHE
In a time 4K0Uo1iWnNa1IzEWGZF928ojiqk1PPX8qGpSXY5qXDXV3KUohrbeLOxS7rxc22ym8QsDBTGHSx3vo2hxDKYkpU1Mqwgb5PZyQsHMGSTb Kaqv E0fsg5RdCwwDiJQPc5gGLtGa0at the same time the fluid at Q moves to R7OIhj0xzSZseP72hHPGDPpCEmx9k82Jmj6 IFEnhRiDWkQDTsnwK2JLCv0sk5dbAVeXiQTcfe4ahCxGp 8n7UkFAS6SrbQaLjMko72c3 IoujRYtil2xcLXfmyNFey91kiQyO8, doing work against the pressure  SvDDRvujy1XY3DOG9QrHr4eTica4v7 V7MDNToTiaApUrFpXfpHFBpqP08qz0TKyxxQ621Gsbz3VVLa6q8ZbJOSl0sXvhXLypAsqzTtPIxLdGrfJ5hUHr0oJX0LMqTZIdMrwo0 at B.
Work done by the fluid against pressure P2
= HSKONAlsySDHCIHi10JmVkPQej9di3W YUtLX52ZY71AY0Aiatst76eCEKObRBxESHVPuzZNq2EsD31ufzTxRyY ZnGoGKGRJ5FEkauLUAE9BiNbbl Q9 Vl B3Ylh7o7WI8GII
Network done on the fluid = work done on the fluid work done by the place
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This equation means, whatever mass of fluid enters the pipe at P in a certain time will leave the pipe at Q at the same time.
Total work done on the fluid = Wnawbone5h F0oAZSygrxfckUW7lfZ6CB KYdH4BzDIEAAAJUX6sxz80c Al2NJkFYKXNcAARzg8C9VMyIsqF9EeqXHvdPLLUQTXcqe142tydtf2MHCbKNWhGEJyJYyozlR8pSw
= (Image?w=67&h=27&rev=1&ac=1&parent=1LROdijXKcU8Ys2KKp6YZtwhvOKDJrPcw
WrYhfkDTY1UFYFjD2cskIQKFTvmuOPH0Mjm69qR9MkQYsMf AfH4sjY2hBPlI4 FEMuMq23RxPut Pa7p5Ls5h36UFq6mwp 826BzvJu5CXDPI164qbdlcFcVdenPIgCQljnUBw
Total energy = ΔK.E + ΔP.E
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Increase in P.E. Image?w=122&h=23&rev=1&ac=1&parent=1LROdijXKcU8Ys2KKp6YZtwhvOKDJrPcw
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Work
done
on
the
fluid =
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From work energy theorem ΔW = ΔK.E + ΔP.E
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QYkDBsxANlvO3DUAEjI U7hKIIr0WhPf9hjoRwhG6SSNqrcuuXN5ggIQOxnRVe2pXd9E90rPoQzIA3mvLbBl3NV2bgRpXpotlkqczfc9 P6UnzawkRe401mz7OpPJ5Ku2GxS40w
S7s76Zh2fCIqmKMmFoyTpzlqalNBxKgypiYhX14zT8hLY3EOjZGr4inlDl61umO5TLfveypcMLxy6Ci6u1ZrvFPOjYTyg5Pj 1lxufb6ERbeFOJfOscjJdLvlkhCkSocL5nU3xY
9ReiCelH3jy6IUlwG VJ1E2tkLiU27Vwuo87e9kjaKgvdRAEr6UlVquW EPZkWgD LiexBqaAPCS4ahr Es8NGcYuB1XkuQkvZ7ok3vddMn1QQYC YKRuoHJTjDmLNfIYFPYmGQ
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FLOW IN A HORIZONTAL PIPE
When the liquid flows through a horizontal pipe
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Hed159d2AW5b9LHB15Gut5tUmssgW7VMumjFQY QjBJ1QCssWTdt Xdsbtkimdmtfq5rP7S XbiwF7pN8MPBdbbAzhAZYckWvHSUX5pjbVI31X1VY ALwdT50LWRNmBBVBszEHAh
Cr7qeDWAAdr1MUEP4oaLFLFGgoBPC6CgUnnkl1CgbLFHlgqmqlYBh8Kl4g KgfxJHfQdTxVnIHj8KxJu6lx7FkvX7tQQSNtdr0qQaG5XnRvQSOjcqEuiD HSRyfS9RTqvO3qowU
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P = Static pressure
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DIFFERENT FORMS OF BERNOULLI’S THEOREM
1. Image?w=301&h=131&rev=1&ac=1&parent=1LROdijXKcU8Ys2KKp6YZtwhvOKDJrPcw
2.
3.
Where by
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LIMITATION OF BRNOLLI’S THEOREM
  1. In derivation of Bernoulli‘s equation, it is assumed that the liquid is non-viscous i.e. the liquid has zero viscosity (no friction).
However, a real liquid does have some viscosity so that a part of mechanical energy is lost to overcome liquid friction. This fact is not taken into account in this elevation.
  1. In derivation of Bernoulli‘s equation, it is assume that the rate of flow of liquid is constant
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But this is not correct in actual practice. Thus in the case of liquid flowing through a pipe, the velocity of flaw is maximum at the center and goes on decreasing towards the walls of the pipe. Therefore, we should take the average velocity of the liquid.
  1. In derivation of Bernoulli‘s equation, it is assumed that there is no loss of energy when liquid is motion. In practice, this is not true e.g. A part of K.E of flowing liquid is converted into heat and is last forever.
  2. If the liquid is flowing along a curved path, the energy due to centrifugal force must be considered.
APPLICATIONS OF BERNOULL’S THEOREM
1. Flow meter – Venturimeter
Is a device that is used to measure the flow speed (flow rate) of a liquid through a pipe. It works on Bernoulli’s theorem.
It consists of two tubes A and C connected by a narrow coaxial tube B with a constriction called the throat.
Using the two tubes D and E the difference in pressure of the liquid flowing through A and B can be round out.
As the liquids flows from A to B the velocity increases, due to decreases in cross-sectional area.
Let the velocities at A and B isV1 and A1 and A2and V2 and cross-sectional areas and A and B be A1 and A2 respectively.
By equation of continuity
A1 V1 = A2V2
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Applying the equation of continuity
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Where Q is the volume of liquid flowing in one second
Applying Bernoulli’s theorem at A and B
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But, A1 > A2, V2> V1 P1> P2hence the level of the liquid in D is higher than that in E.
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H – Difference of levels of the liquid in the tubes D and E.
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TORRICELLI’S THEOREM
States that “if the difference in levels between the hole and the upper liquid surface in a drum is h, then
the velocity with which the liquid emerges from the hole in CwdaEy1OmzSCvZdGYPU32tCEaIZonSnIfhePg1UojVDQv6uo2L25qMyIcwjmnrPp51ek8hrab5KD0VJPEy N4h3gz68mk 5KYB088AswYn1V5o7Cz3WnSGSksuKY52GxEWxRaYk States that the velocity of efflux is equal to the velocity which a body attains. in falling freely from the surface of the liquid to the orifice
Velocity of efflux
Is the velocity of liquid at the orifice.
Or
Is the velocity of emerging fluid from the orifice
This theorem applies to a liquid flowing from a drum with a horizontal opening near the base.
This is the same velocity which freely falling object will acquire in falling from rest through a vertical distance h.
PROOF OF TORRICELLI’S THEOREM
Suppose an ideal liquid flows through a hole H at the bottom of a wide drum as shown below
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Let BdsZzDzUC0 QTzvFiGV6UqT4l6AMygt0ZBwvudUGnGdhwf1RdCjXjCYbBsniQKv7KVvVrOuOtYW KlFU1rpnt9MgUAg4efbdAtWetXiNCCWWvjEvGTJVwxSO5aYYFJ4eq39qwIbe the density of the liquid.
According to Bernoulli’s theorem, at any point of the liquid
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At point 1
The point 1 is at the surface of the liquid in the drum
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At point 2
The point 2 is at the place where liquid leaves the hole.
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*The velocity of the liquid emerging from the hole depends only upon the depth h of the hole below the surface of the liquid.
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Horizontal Range
The liquid flows out of the hole in the form of a parabolic jet and strikes the ground at a distance R from the base of the drum.
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The distance R is the horizontal range of the liquid coming out of the hole.
At the hole P, the velocity V2 of the emerging liquid is along the horizontal direction.
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T – Time taken by the parabolic jet to strike the ground after emerging from the hole P h1 – Height of hole above the bottom of the drum
Therefore, the vertical distance covered by the set in time T is h
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PITOT TUBE.
Pitot tube is a device used for measuring the velocities of flowing liquids and hence the rates of flow of the liquids.
Its working is based on Bernoulli’s theorem.
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Pitot tube is an open ended L-shaped tube immersed in the liquid with its aperture and its nose B facing the flow of liquid, so that the plane of the aperture is normal to the direction of another tube A with a small opening at its bottom.
The plane of aperture of A is parallel to the direction of flow, so that it measures the static pressure 8ap1db7zS7VBMZMVlrPB Yn3Fft9jCjhz NDo61ghx0NGG82P DHqa7AMw6Y5UroOVhGHjXkJ0AyD3Bj T7 HCBjkG Yi9n0oXqBgAyHKku6019mrBkl5EEvBzuelWue15j7MJE at A, which is the pressure of the undisturbed liquid.
The flow of liquid is stopped in the plane of aperture B, there by converting the Kinetic energy of the liquid into P.E.
So the liquid rises in the tube T as shown. The height of the liquid in this tube gives the total pressure or the stagnation pressure.
Applying Bernoulli’s Equation
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Let the difference between the levels of the liquid in the two tubes be h
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The velocity of flow of the liquid
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The rate of flow of liquid
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A – Area of cross-sectional of the pipe at the place where the pitot tube is placed.
Static pressure.
Static pressure is the actual pressure of the fluid at the point due to its rest position of fluid.
Dynamic pressure.
Dynamic pressure is the pressure exerted by fluid due to its own motion.
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Let h be difference in the liquid levels in the two limbs.
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