Es2c50 sol - Solutions to Year2 past papers from the 2019 series PDF

Title Es2c50 sol - Solutions to Year2 past papers from the 2019 series
Author Vick vi
Course Dynamics and Fluid mechanics
Institution The University of Warwick
Pages 8
File Size 541.5 KB
File Type PDF
Total Downloads 264
Total Views 376

Summary

UNIVERSITY OF WarwickSchool of EngineeringYear 2June 2019ES2C5 Title of Examination: -DYNAMICS AND FLUID MECHANICSPage 1Question 1MarkAllocation***************************************** Begin 1 *******************************************(a) Given: = 2 ms , = 0 m, = 5 N, = 1 m, = 1 × 10, = 1 × 10,= 9...


Description

Year 2 June 2019

UNIVERSITY OF Warwick School of Engineering ES2C5

Title of Examination: DYNAMICS AND FLUID MECHANICS

Page 1

Question 1

Mark Allocation

***************************************** Begin 1 ******************************************* (a) Given:  = 2 ms  ,  = 0.08 m,  = 5 N,  = 1.5 m,  = 1.3 × 10 



 = 999 kgm , density air,  = 1.23 kgm



,  = 1.46 × 10

 , 

Marks *** B1 ***

(i) For dynamic similarity the Reynolds numbers for the sphere in water and the balloon must be the same. Reynolds number sphere in water:  = Therefore, for balloon  =

  

  

=

= 123,077

  .  .×

 

= 123,077 ≈ 1.2 × 10 

 =  123,077





=

 

.× . 

123,077 = 1.198

 

≈ 1.2

 

3 marks

(ii) For equal Reynolds number / Dynamic similarity the drag coefficients for sphere and balloon will be the same. Find drag coefficient for sphere     = 0.498  =   =  = =     .         



  (  )

󰇡

󰇢





 

( 

. 

)

. 

Thus,  =  = 0.498 and with this value it follows for balloon that 

 =      = 0.498

 

1.23 kgm (1.2 ms  )  󰇡

(b) Given:  = 0.18 m,  = 0.13 m,  = 0.5 m s  ,  = 12 ms 

.   

󰇢 = 0.779 N

.  

Calculate volumetric flow rate going out at section (2)  =    =  󰇡  󰇢 12 ms  = 0.305 m s  Mass conservation requires:  =  +  →  =  −  = 0.5 m s  − 0.305 m s  = 0.195 m s  Since  <  it follows the flow velocity at section (3) must be directed outwards. (Note: We could have formally assigned minus sign to ‘In’ velocities and plus sign to ‘Out’ velocities to arrive at this result but it is unlikely that any student will do this. Now find average velocity at section (3):  =





=

.  .   󰇡 󰇢 

=

.  . 

= 14.7 ms 

3 marks

1 marks 2 marks 1 mark 2 marks

(c) Assume linear velocity profile between cylinder an pipe wall and apply Newton’s law of viscosity. The resulting shear stress on the surface of the cylinder will be in equilibrium with the force of gravity on the cylinder at the condition of terminal speed. From data in figure from question we conclude that the gap with between cylinder and pipe is equal to: 1 h  74 mm  73.8 mm   0.1 mm 2 V Shear stress from Newton’s law of viscosity:    T h For shear force, F s , resisting downward motion need to multiply by surface area of cylinder

F s   D L  

VT h

Fg  m g

Downward gravitational force F g is: When terminal velocity is reached we have:



Fs  Fg

m g   D L  

VT h

6 marks



mg h VT     D L 

2.5 kg 9.81 7  10

-3

Ns m

0.0024525

2



m s2

0.0001 m

0.074 m 0.15 m 

kg m2

s 2  10.05 m 0.000244101 N s s (Note: The downward moving cylinder acted on only by viscous friction from the oil film and by gravity never reaches so-called terminal velocity unless we allow, theoretically, an infinite span of time.) 

(d) Given densities:  W  998 kg m 3; steel,  S  8,000kg m 3 ; mercury,  M  13,550kg m 3 For the block to float the weight of the liquid it displaces must equal its own weight. Weight block: W B  l  d  a  b  S g Weight displaced liquid: W L  l d  a  W g  l  d  b  M g Equating both:

l  d  a  b  S g  l  d  a W g  l  d  b  M g a  b  S  a W  b  M   a  S  b s  a  W  b  M   

2 marks

1 mark 1 mark 2 marks

a  S  a  W  b  M  b s a   S   W   b  M   s  a  b

M S

  s  13,550  8,000  5550    0.79  W  8,000  998 7002

****************************************** End 1 *******************************************

1 mark

*** E1 ***

***************************************** Begin 2 ****************************************** (a) The fundamental dimensions are: Mass M , Length L , Time T . The dimensions of the quantities involved in the problem are: M M L Velocity , Density 3 , Surface Tension (= Force/Length) 2 . T L T (1) The problem formulation states We  l  F (V ,  , )

We  l  V      

Now assume

 L Introducing dimensions in (2) yields We L 1   T  From this one gets









M  M    3   2   L  T 



M 0 L0T 0  L   LT    M  L3   M T  2  1

 

1  3 

combining corresponding terms M L T  M L Comparing the corresponding exponents yields from M : 0   (I), from L : 0 1 3 (II), (III). from T : 0   2 0

Resolving (I) for this in (II) yields

(2)

0

0

T

*** B2 ***

1 mark

2 marks



1 mark



1 mark

  2

2 marks

 , introducing this in (II) and then resolving (III) for 

and also introducing

01  2 3    1   such that    1 . With (I) and (III) one then finds   1 and   2 . lV   2

With (2) the final solution is thus

We

1 mark

3 3 (b) Given: density mercury,  M  13,550 kg m ; density water, W  998 kg m , D1  7.5 cm , D2  2.5 cm , h1  60 cm , h2  3 m

Establish ejection velocity by continuity:

V1 A1  V2 A2



V2  V1

A1 A2

 V1

D    1   2 

2

D    2   2 

2

 V1

D12 D22

m 0.075 m 

2

 0 .5

s

0.025 m 

2

 4 .5

m

Now apply Bernoulli between station (1) and (2) to establish pressure at station (2)   p 1  w V12   W gz1  p 2  W V 22  W gz 2 2 2 where we use height at station (1) as datum such that z 1  0 and z 2  3 m and p 2  0 . With Eq. (A) we have kg kg 998 3 998 3 2 2 m   m 0.5 m  4.5 m   998 kg 9.81 m 3 m p1     0  0   2 2  s s   s2 m3

kg kg 998 3 2 2 3  m m m kg  m m 0 . 5 3 m 4 . 5 9 . 81 998  p1       2  2  s s s2 m3 p1  10,105 Pa  29,371 Pa  125 Pa  39,351 Pa This result for p 1 is gauge pressure. Now, the manometer reads gauge pressure.  M gh p1  W gh1 Hence, 998

p1 p1  gh   W 1   W h1 M g M g M g  M kg 998 3 p1 39,351 Pa  W gh1 m h    0.6 m  0.3 m  0.04 m  0.34 m kg m kg M g  Mg 13,550 3 9.81 2 13,550 3 m s m h



2 marks

s

(A)

3 marks

1 mark

2 marks

1 mark

(c) Neglect gravity and assume that for a free jet the pressure is constant everywhere. Control volume is indicated in figure in question. Use R for force exerted by the fluid on the vane and F   R for force by vane on fluid. Component forces Fx and F y in the x and y are 

F x  m1 v out  v in  x



Fy  m 2 v out  v in  y

and similarly 





Since nozzle and vane are fixed relative to each other, m1  m2  m In

Fx  0.8

kg  m m kg  m m kg  m  kg m o  17,5   14 2  14 N 25 cos 60  30   0.8  12.5  30   0.8 s  s s  s  s s s  s  s v in  0

In y direction:

Fy  0.8

and v out  v 2 cos

v in  v1

x direction:

and

v out  v 2 sin

m kg  m m kg     25 sin 60 o  0   0.8  25 0.866 s s  s s s   kg m m  kg    17.32 2  17.32 N   21.65 s  s  s R x  14 N and R y  17.32 N  0.8

Hence,

7 marks

Combining R x and R y :gives resultant force R

 R x 2  R y 2

This resultant force will be inclined to the

  tan  1

Rx Ry



14 N 2  17.32 N 2

 495.98 N 2  22.27 N

x direction at an angle

 tan  1

17.32  tan  1 1.237  51.05o 14

****************************************** End 2 *******************************************

1 mark

*** E2 ***

UNIVERSITY OF Warwick School of Engineering ES2C5

Title of Examination: DYNAMICS AND FLUID MECHANICS

Question 3

***************************************** Begin 3 ******************************************* (a)

Year 2 Jan 2019 1 Mark Allocation Marks *** B3 ***

i)

Potential Energy: V = mgh Kinetic Energy: KE = ½mv2

2 marks

Potential energy of mass when y=0.4 is then: 1 mark

To find KE at y=0.4, use principle of work and energy: P.E. + K.E. = const. Potential energy at y=0 Kinetic energy at y=0

Principle of work and energy: Therefore:

2 marks

ii) Maximum height occurs (ymax) when KE=0. Principle of work and energy: reduces to: Therefore and

3 marks

iii)

W ork done by force, F, tangential to direction of motion:

In this question, F=-2 N, and so U=-2s When y=0.4, s =0.8 m Therefore 2 marks

UNIVERSITY OF Warwick School of Engineering ES2C5

Title of Examination: DYNAMICS AND FLUID MECHANICS

Question 3

Year 2 Jan 2019 Page 2 Mark Allocation Marks

iv)

When non-conservative forces act, the pri nciple of work and energy is: Where U is work done by non-conservative forces (negative in the case of friction) And so: Rearranging gives: 4 marks (b) i)

Firstly find the instantaneous centre:

4 marks

ii) The angular velocity of the bar is given by:

3 marks

1.45 rad/s iii)

The velocity magnitude at B is: 2 marks

m/s iv) the magnitude of centrpetal acceleration at A:

aA / IC ,r = -w 2 r = (1.45 2 ) ´ 0.173 = 0.364 m/s 2

***************************************** End 3 *******************************************

2 marks

*** E3 ***

UNIVERSITY OF Warwick School of Engineering ES2C5

Title of Examination: DYNAMICS AND FLUID MECHANICS

Question 4

Year 2 Jan 2019 Page 3 Mark Allocation

***************************************** Begin 4 *******************************************

Marks *** B4 ***

i) Kinetic energy of the system as a whole: 





 

K.E.=    +    +  󰇡 󰇢 = 2.55     

5 marks

ii) Potential energy of the system as a whole (note, extension of the upper spring = 2 x)

2 marks





P.E.= −( +  ) + (2 ) +    = −49.1 + 125  

4 marks

iii) Principle of work and energy: P.E. + K.E. = const

Therefore, 2.55  − 49.1 + 125  = 

1 mark

Differentiate with respect to time: 2.55 2

    − 49.1 + 125 2  = 0   

Since v=dx/dt, we can write 5.1

      =0 − 49.1 + 250     

Dividing through gives: 5.1

  + 250 = 49.1 

The characteristic equation (i.e. redefining x to be displacement away from equilibrium) is:

  5.1  + 250 = 0 

4 marks

and assuming vibration of the form  =  we get: 

 =  . = 7 rad/s

3

3 marks

UNIVERSITY OF Warwick School of Engineering ES2C5

Title of Examination: DYNAMICS AND FLUID MECHANICS

Question 4 contd Marks

1 marks

2 marks

3 marks

***************************************** End 4 *******************************************

*** E4 ***...


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