Isentropic flow of an ideal gas with k =1.4
10
0.9
9
0.8
8
0.7
7
0.6
6
T /T0
; /; 0
p /p0
0.5
5
A/A *
0.4
4
0.3
3
0.2
2
0.1
1
0
10 -1
10 0
Mach Number
0
10 1
Area Ratio
Property Ratios
1
Normal shock flow of an ideal gas with k =1.4
1
40
0.9
p0y /p0x
p0y /px
0.8
py /px
; y /; x
35
30
Ty /Tx
0.7
25
0.6
0.5
20
0.4
15
0.3
10
0.2
5
0.1
0
1
1.5
2
2.5
3
3.5
4
Mach Number before Shock
4.5
5
0
p0y /px , py /px , ; y/; x , Ty /Tx
Mach Number after Shock and p0y /p0x
May
5
Fanno flow of an ideal gas with k =1.4
2.5
p /p*
p0 /p*0
2
3
1.5
2
1
1
0.5
f (L* - L )/D
Property Ratios
4
T /T*
; * /;
f (L* - L )/D
0
10 -1
10 0
Mach Number
0
10 1
p /p* , T /T* , ; * /;
2
Rayleigh flow of an ideal gas with k =1.4
p /p*
T /T*
; * /;
p0 /p*0
T0 /T*0
5
4
1.5
3
1
2
0.5
1
0
10 -1
10 0
Mach Number
0
10 1
p0 /p*0 , T0 /T*0
2.5