894 ENGINEERING THERMODYNAMICS
dharm
\M-therm\Th16-2.pm5Mach number, M 2 :M 22 =()
()γ
γγ−+
−−12
211
2
1
2M
M
...[Eqn. (16.49)]=
()
()1.4
1.4 1.43.6
11.2 0.4−× +
××− −=
−12 2
22 12
2 = 0.333
∴ M 2 = 0.577 (Ans.)
Pressure, p 2 :
p
p2
1=21
11
γγ^2
γM −−
+()
() ...[Eqn. (16.46)]=
2142 141
14 111 2 0 4
24××− −^2
+.(.)= −
(. )... = 4.5
∴ p 2 = 26.5 × 4.5 = 119.25 kN/m^2 (Ans.)
Density, ρ 2 :
ρ
ρ
2
1
=()
()γ
γ+
−+1
121
2
1
2M
M ...[Eqn. (16.47)]= (. )
(. ).
.14 1 2
14 1 2 296
16 22
2+
−+=
+= 2.667∴ ρ 2 = 0.413 × 2.667 = 1.101 kg/m^3 (Ans.)
Temperature, T 1 :Since p 1 = ρ 1 RT 1 , ∴ T 1 =p
R1
ρ 1
=
26 5 10
0 413 287.^3
.
×
× = 223.6 K or – 49.4°C (Ans.)
Temperature, T 2 :
T
T2
1= [( ) ] [ ( )]
()[( ) ] [ ( )]
()γγγ
γ−+ −−
+= −+ ××−−
+122 1
112 2 2 2 1
1212 12
2 1222
22MM
M1.4 1.4 1.4
1.4= (. )(..
.16 2 112 0 4)
23 04+− = 1.6875∴ T 2 = 223.6 × 1.6875 = 377.3 K or 104.3°C (Ans.)
Velocity, V 1 :
C 1 = γRT 1 = 1 4 287 223 6..×× = 299.7 m/sSinceV
C1
1= M 1 = 2 ∴ V 1 = 299.7 × 2 = 599.4 m/s (Ans.)
Velocity, V 2 :
C 2 = γRT 2 = 1 4 287 377 3..×× = 389.35 m/sSinceV
C2
2= M 2 = 0.577 ∴ V 2 = 389.35 × 0.577 = 224.6 m/s (Ans.)