SOLUTION MANUAL
, TABLE OF CONTENTS
INTRODUCTION ................................................................................................................... 1
COMPUTER PROBLEMS .................................................................................................... 2
Standard Programs-File Names and Use .................................................................... 2
SOLUTIONS
Chapter 1 Introduction................... .......... ............. ..................... ....................... 1-1
Chapter 2 Fluid Statics......... ..... ...... ........ ................ .......................................... 2-1
Chapter 3 Elementary Fluid Dynamics-Bernoulli Equation .......................... 3-1
Chapter 4 Fluid Kinematics... ...... .......... ......... ..... ................... .......................... 4-1
Chapter 5 Finite Control Volume Analysis ....................................................... 5-1
Chapter 6 Differential Analysis of Fluid Flow ................................................. 6-1
Chapter 7 Similitude, Dimensional Analysis, and Modeling ............ ............... 7-1
Chapter 8 Viscous Pipe Flow............................................ ................................ 8-1
Chapter 9 Flow Over Immersed Bodies ........................................................... 9-1
Chapter 10 Open-Channel Flow...... ...... ......... ....... ..................................... ...... 10-1
Chapter 11 Compressible Flow ......................................................................... 11-1
Chapter 12 Turbomachines ............. .................. ................................................ 12-1
Appendix A Listing of Standard Programs .......................................................... A-I
,t. t I
1..1 Detennine the dimensions. in both the FLT system and
the MLT system, for (a) the product of mass times velocity,
(b) the product of force times volume. and (c:) kinetic energy
divided by area,
1
mASS ;( ve/oc;'& .:. (;VI ) (L 7- ) -
Sinee. F .:. M L T-.2
Fr
=
( b) ./oree J( Y&/I/ml! - F L3
_ (ML T-2.)(L3) _ /'1L if T-Z.
(~ ) J::,;'e/:'G e ne r.!~
t:l reL
-2.
/'1T
/- I
, /'2
1.2 Verify the dim~nso, in both the FLT
and MLT~ystem .. ofthe folioWing quantities which
appear in Table 1.1: (a) angular velocity, (b) en-
ergy, (c) moment of inertia (area), (d) power,
and (e) pressure.
( 0.) = a 1'19 tI //1 r c/'spkce/?'J()~; ..!.
-time
(.b) e he 1'"1:J ~ C.a.;aci +!J 01 b~cJ!1 1-0 do w()rk
Since. Wt?/'"K = I()rce;( d/sl-tll1tt:..)
~nerJ! ; FL
tJr ~if;, F _' /11 L T- 2
e. n erj tj ~ (M I- T -2) (L) == M L 2 T - 2
cc) /7l{pmfl1t 0/ inerlt.~V'a) = sec~l?d /nl'Jme/}f D/ t:lff?l
. (1.:2-)L~ =. L If
. L- 2
= +-()rce
- ~
, .£
LZ. =F
J..---------- - - - - - - - - - - - - - - - - - - - - - - -
/-2.