sid_galt said:
Two identical fuel/air mixtures are kept in boxes A and B at equal pressure, volume and temperature. The mixture in box A is burnt using a subsonic flame. The mixture in box B is detonated. Which will generate more pressure and temperature?
If fuel/air mixture is forced into a chamber containing high pressure gas (20 atm) at high temp, will the mixture deflagrate or detonate?
The answer to this question is not a trivial one. First of all, the detonation conditions are dependant on the nature of the fuel. So it would be impossible to forecast if it will be a detonation or a deflagration if you don't say what fuel are we talking about. Also, detonation processes are very influentiated on how are they initiated. In your example, there must be reached detonation conditions during the chemical reaction of explosion, and this achievement is studied taking into account the heat transfer properties of the vessel. You know, there are also depurated techniques for fabricating explosive vessels, taking into account the ratio of heat chemically released and the heat transferred to vessel surroundings.
The main differences between a deflagrative and a detonative wave are:
i) a detonative wave travels at supersonic velocity. In fact it is a reactive shock wave. It is used in pulsed detonation engines because behind the front of a detonative wave, the pressure and temperature of products are higher than the reactants pressure, so it will push air to rearwards, pushing also the engine by pressure.
ii) a deflagrative wave travels at subsonic velocity. For example, a deflagrative wave is the wave produced by a bunsen burner. It is a steady diffusion flame, but viewed from a reactant reference frame, it is a wave which travels far below sonic limit. On the other hand, deflagrative waves causes a decreasing of pressure behind it, they expand the gases. This deflagrative waves can be seen at explosions in buildings and firings. Deflagrative waves are not reliable for scramjet engines, because the flow is supersonic at the inlet, but they are produced in usual turbojet engines and ramjets.
Astronuc said:
If the total energy is the same and the mass involved is the same, and it is purely adiabatic (i.e. no heat loss), then yes the final temperature would be the same.
Today 06:42 PM
I don't think so. Both processes deflagrations and detonations are non isentropic ones. Moreover, I will leave sid-galt to demonstrate that a detonation process causes more increasing in entropy. It can be seen graphically with Rankine-Hugoniot curves or analitically. Surprisingly, detonation processes are more difficult to achieve in a naturally way. They must be forced, unless the mixture reaches detonation conditions. So that, a detonation will cause greater final temperature.
For more references, you all can take a look at the book of my signature. It is written by FA Williams (UCSD) and A. Liñan (ETSI Aeronauticos Madrid). A great book

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