894 ENGINEERING THERMODYNAMICS
dharm
\M-therm\Th16-2.pm5
Mach number, M 2 :
M 22 =
()
()
γ
γγ
−+
−−
12
21
1
2
1
2
M
M
...[Eqn. (16.49)]
=
()
()
1.4
1.4 1.4
3.6
11.2 0.4
−× +
××− −
=
−
12 2
22 1
2
2 = 0.333
∴ M 2 = 0.577 (Ans.)
Pressure, p 2 :
p
p
2
1
=
21
1
1
γγ^2
γ
M −−
+
()
() ...[Eqn. (16.46)]
=
2142 141
14 1
11 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
12
1
2
1
2
M
M ...[Eqn. (16.47)]
= (. )
(. )
.
.
14 1 2
14 1 2 2
96
16 2
2
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
R
1
ρ 1
=
26 5 10
0 413 287
.^3
.
×
× = 223.6 K or – 49.4°C (Ans.)
Temperature, T 2 :
T
T
2
1
= [( ) ] [ ( )]
()
[( ) ] [ ( )]
()
γγγ
γ
−+ −−
+
= −+ ××−−
+
122 1
1
12 2 2 2 1
12
12 12
2 12
22
22
MM
M
1.4 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/s
Since
V
C
1
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/s
Since
V
C
2
2
= M 2 = 0.577 ∴ V 2 = 389.35 × 0.577 = 224.6 m/s (Ans.)