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6.13. Using thermite for soldering rails. The temperatures attained durin...Figure 6.14. a) Schematic of a solid propellant rocket (source: https://fr.wikip...Figure 6.15. Schema for the combustion of an aluminum particle in a propellant e...Figure 6.16. Propagation of a discrete combustion wave in multilayer spin mode (...Figure 6.17. Spray combustion: a) individual drop combusting with a spherical di...Figure 6.18. Traces of the droplet paths illustrating the continuous cascading f...Figure 6.19. Control volume (V), the normal n is at boundary(∂V)Figure 6.20. Discontinuity interface. The normal N to the discontinuity is orien...Figure 6.21. 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
5 Preface
8 Index
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