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Untitled - Aerobib - Universidad Politécnica de Madrid

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5.5. DETONATIONS 119<br />

This relation shows that the pressure at each point of the wave is <strong>de</strong>termined<br />

only by the corresponding value of the <strong>de</strong>nsity. This relation plays here the same part<br />

as, for example, in Gas Dynamics the relation p = Cρ γ for the isentropic motions of<br />

non-reacting gases.<br />

In or<strong>de</strong>r to represent the result in the diagram (p, τ), as done in chapter 3, the<br />

specific volume τ = 1/ρ must be introduced in place of the <strong>de</strong>nsity in Eq. (5.39),<br />

which then takes the form<br />

p − p 1 = m 2 (τ 1 − τ). (5.40)<br />

This equation is represented in diagram (p, τ), see Fig. 5.2, by a straight line joining<br />

the representative points of the initial and final states. On this line also lie all the<br />

representative points of the intermediate states corresponding to the reaction zone. 11<br />

70<br />

60<br />

D<br />

p/p 1<br />

E<br />

50<br />

C<br />

Trayectory through shock wave<br />

40<br />

30<br />

ε=1.0<br />

J<br />

20<br />

E‘<br />

ε=0.3 ε=0.7<br />

10<br />

ε=0<br />

1<br />

P<br />

0.0 0.2 0.4 0.6 0.8 1.0<br />

τ /τ 1<br />

Figure 5.2: Hugoniot curves from different values of ε.<br />

Bringing forth in Eqs. (5.1.a), (5.28.a) and (5.29.a) the specific volume and the<br />

initial conditions corresponding to the unburnt gases, there results<br />

v<br />

τ = v 1<br />

τ 1<br />

, (5.41)<br />

p + v2<br />

τ = p 1 + v2 1<br />

τ 1<br />

, (5.42)<br />

c p T + 1 2 v2 − qε = c p T 1 + 1 2 v2 1. (5.43)<br />

11 W. Michelson was the first to postulate that within the reaction zone of the <strong>de</strong>tonation wave the linear<br />

relation (40) is verified.

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