Visualizations of shocks. a) Normal shock in the divergent part of ...Figure 6.22.
a) Diagram of a Laval nozzle with a shock in the divergent part. b)...Figure 6.23. Motion on either side of the piston with uniform velocity VP. The t...Figure 6.24.
The Hugoniot adiabatic in the planes a) ϑ
, p and b) | s. The Mach n...Figure 6.25. a) The flow rate line (in both cases) M1 = u1/c1 denoting the Mach ...Figure 6.26. Rankine–Hugoniot configuration: representation of the steady motion...
Guide
1
Cover
2
Table of Contents
3
Title Page
4
Copyright
5
Preface
6
Begin Reading
7
List of Authors
8
Index
9
Summary of Volume 2
10
End User License Agreement
Pages
1
v
2
iii
3
iv
4
ix
5
x
6
xi
7
1
8
2
9
3
10
4
11
5
12
6
13
7
14
8
15
9
16
10
17
11
18
12
19
13
20
14
21
15
22
16
23
17
24
18
25
19
26
20
27
21
28
22
29
23
30
24
31
25
32
26
33
27
34
28
35
29
36
30
37
31
38
32
39
33
40
34
41
35
42
36
43
37
44
38
45
39
46
40
47
41
48
42
49
43
50
44
51
45
52
46
53
47
54
48
55
49
56
