FLUID MECHANICS >C<
FLUID MECHANICS >C<
18th Edition
ISBN: 9781308529622
Author: White
Publisher: MCG/CREATE
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Chapter 8, Problem 8.45P
To determine

(a)

The value of K for which the cavitation will begin at surface.

Expert Solution
Check Mark

Answer to Problem 8.45P

The value of K for which the cavitation will begin at surface is Kcavitation=4.4m2/s.

Explanation of Solution

Given information:

Free stream velocity U=6m/s

The value of pressure outside the boundary layer p=200kpa

The density of water at 20° C = ρ=998kgm3

The vapor pressure of water at 20° C = pvap=2337pa

Calculation:

The expression of velocity at the surface is given by

Vsurf=2Usinθ+K0.5

Putting the values,

Vsurf=2×6sinθ+K0.5

At the stagnation conditions the velocity becomes zero, at the stagnation point the pressure is po=218000pa . At θ=270o, applying Bernoulli’s equation.

p0=pvap+ρ2(Vsurf)2

Putting the values in the equation:

218000=2337+9982(2×6×sin(270)+K0.5)

From the above equation, the value of K is Kcavitation=4.4m2/s.

Conclusion:

Thus, the value of K for which the cavitation will begin at surface is Kcavitation=4.4m2/s.

To determine

(b)

The point where the cavitation will begin.

Expert Solution
Check Mark

Answer to Problem 8.45P

The cavitation will begin at the point where the pressure is lowest.

Explanation of Solution

A point in the fluid flow where pressure drops to such a value that it becomes equal to the atmospheric pressure is called the point of cavitation. The pressure is lowest at this point in the fluid flow.

In present fluid flow the pressure drops to the lowest value at the bottom most shoulder. The value of angle at this point is θ=270o.

To determine

(c)

The place of stagnation points.

Expert Solution
Check Mark

Answer to Problem 8.45P

The stagnation points lie at two locations θstag=47oand133o

Explanation of Solution

Given information:

Free stream velocity U=6m/s

The value of pressure outside the boundary layer p=200kpa

The density of water at 20° C = ρ=998kgm3

The vapor pressure of water at 20° C = pvap=2337pa

Calculation:

The expression of velocity at the surface is given by:

Vsurf=2Usinθ+K0.5

Putting the values,

Vsurf=2×6sinθ+K0.5

At the stagnation conditions the velocity becomes zero, at the stagnation point the pressure is po=218000pa . At θ=270o, applying Bernoulli’s equation:

p0=pvap+ρ2(Vsurf)2

Putting the values in the equation:

218000=2337+9982(2×6×sin(270)+K0.5)

From the above equation, the value of K is Kcavitation=4.4m2/s

Now, from the value of K, the location of stagnation points can be found from the following equation:

sinθstag=K2Ua

Now, putting values in the above equation gives:

sinθstag=4.42×6×0.5=0.732

This gives two values of angle θstag=47oand133o.

Conclusion:

Thus, stagnation points lie at two locations θstag=47oand133o.

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Chapter 8 Solutions

FLUID MECHANICS >C<

Ch. 8 - Prob. 8.11PCh. 8 - Prob. 8.12PCh. 8 - P8.13 Starting at the stagnation point in Fig....Ch. 8 - P8.14 A tornado may be modeled as the circulating...Ch. 8 - Hurricane Sandy, which hit the New Jersey coast on...Ch. 8 - Prob. 8.16PCh. 8 - P8.17 Find the position (x, y) on the upper...Ch. 8 - Prob. 8.18PCh. 8 - Prob. 8.19PCh. 8 - Plot the streamlines of the flow due to a line...Ch. 8 - P8.21 At point A in Fig. P8.21 is a clockwise line...Ch. 8 - P8.22 Consider inviscid stagnation flow, (see...Ch. 8 - P8.23 Sources of strength m = 10 m2/s are placed...Ch. 8 - P8.24 Line sources of equal strength m = Ua, where...Ch. 8 - Prob. 8.25PCh. 8 - Prob. 8.26PCh. 8 - Prob. 8.27PCh. 8 - Sources of equal strength m are placed at the four...Ch. 8 - Prob. 8.29PCh. 8 - Prob. 8.30PCh. 8 - A Rankine half-body is formed as shown in Fig....Ch. 8 - Prob. 8.32PCh. 8 - P8.33 Sketch the streamlines, especially the body...Ch. 8 - Prob. 8.34PCh. 8 - Prob. 8.35PCh. 8 - Prob. 8.36PCh. 8 - Prob. 8.37PCh. 8 - Consider potential flow of a uniform stream in the...Ch. 8 - A large Rankine oval, with a = 1 m and h = 1 m, is...Ch. 8 - Prob. 8.40PCh. 8 - Prob. 8.41PCh. 8 - Prob. 8.42PCh. 8 - P8.43 Water at 20°C flows past a 1-rn-diameter...Ch. 8 - Prob. 8.44PCh. 8 - Prob. 8.45PCh. 8 - P8.46 A cylinder is formed by bolting two...Ch. 8 - Prob. 8.47PCh. 8 - Prob. 8.48PCh. 8 - Prob. 8.49PCh. 8 - It is desired to simulate flow past a...Ch. 8 - Prob. 8.51PCh. 8 - P8.52 The Flettner rotor sailboat in Fig. E8.3...Ch. 8 - P8.52 The Flettner rotor sailboat in Fig. E8.3 has...Ch. 8 - Prob. 8.54PCh. 8 - Prob. 8.55PCh. 8 - Prob. 8.56PCh. 8 - Prob. 8.57PCh. 8 - Prob. 8.58PCh. 8 - Prob. 8.59PCh. 8 - Prob. 8.60PCh. 8 - Prob. 8.61PCh. 8 - Prob. 8.62PCh. 8 - The superposition in Prob. P8.62 leads to...Ch. 8 - Consider the polar-coordinate stream function...Ch. 8 - Prob. 8.65PCh. 8 - Prob. 8.66PCh. 8 - Prob. 8.67PCh. 8 - Prob. 8.68PCh. 8 - Prob. 8.69PCh. 8 - Prob. 8.70PCh. 8 - Prob. 8.71PCh. 8 - Prob. 8.72PCh. 8 - Prob. 8.73PCh. 8 - Prob. 8.74PCh. 8 - Prob. 8.75PCh. 8 - Prob. 8.76PCh. 8 - Prob. 8.77PCh. 8 - Prob. 8.78PCh. 8 - Prob. 8.79PCh. 8 - Prob. 8.80PCh. 8 - Prob. 8.81PCh. 8 - Prob. 8.82PCh. 8 - Prob. 8.83PCh. 8 - Prob. 8.84PCh. 8 - Prob. 8.85PCh. 8 - Prob. 8.86PCh. 8 - Prob. 8.87PCh. 8 - Prob. 8.88PCh. 8 - Prob. 8.89PCh. 8 - NASA is developing a swing-wing airplane called...Ch. 8 - Prob. 8.91PCh. 8 - Prob. 8.92PCh. 8 - Prob. 8.93PCh. 8 - Prob. 8.94PCh. 8 - Prob. 8.95PCh. 8 - Prob. 8.96PCh. 8 - Prob. 8.97PCh. 8 - Prob. 8.98PCh. 8 - Prob. 8.99PCh. 8 - Prob. 8.100PCh. 8 - Prob. 8.101PCh. 8 - Prob. 8.102PCh. 8 - Prob. 8.103PCh. 8 - Prob. 8.104PCh. 8 - Prob. 8.105PCh. 8 - Prob. 8.106PCh. 8 - Prob. 8.107PCh. 8 - P8.108 Consider two-dimensional potential flow...Ch. 8 - Prob. 8.109PCh. 8 - Prob. 8.110PCh. 8 - Prob. 8.111PCh. 8 - Prob. 8.112PCh. 8 - Prob. 8.113PCh. 8 - Prob. 8.114PCh. 8 - Prob. 8.115PCh. 8 - Prob. 8.1WPCh. 8 - Prob. 8.2WPCh. 8 - Prob. 8.3WPCh. 8 - Prob. 8.4WPCh. 8 - Prob. 8.5WPCh. 8 - Prob. 8.6WPCh. 8 - Prob. 8.7WPCh. 8 - Prob. 8.1CPCh. 8 - Prob. 8.2CPCh. 8 - Prob. 8.3CPCh. 8 - Prob. 8.4CPCh. 8 - Prob. 8.5CPCh. 8 - Prob. 8.6CPCh. 8 - Prob. 8.7CPCh. 8 - Prob. 8.1DPCh. 8 - Prob. 8.2DPCh. 8 - Prob. 8.3DP
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