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A review of the dense Z-pinch

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Plasma Phys. Control. Fusion 53 (2011) 093001<br />

Topical Review<br />

and τ 0 is (4πM l a0 2/µ 0A 2 ) 1/4 as before. It can be seen that <strong>the</strong> implosion is slower because<br />

all <strong>the</strong> mass is initially concentrated at <strong>the</strong> radius a 0 , and <strong>the</strong> shell arrives on <strong>the</strong> axis at <strong>the</strong><br />

dimensionless time <strong>of</strong> 1.752. This was found from a series solution in y up to power <strong>of</strong> y 20 ,<br />

where in a series similar to equation (4.3) only terms in powers <strong>of</strong> y 4 exist, <strong>the</strong> coefficient <strong>of</strong><br />

y 4 being 1/12 and <strong>of</strong> y 8 1/672.<br />

However <strong>the</strong> current waveform for Z at Sandia and for MAGPIE at Imperial College is<br />

more closely <strong>of</strong> <strong>the</strong> form<br />

( ) πt<br />

I = I 0 sin 2 , (4.16)<br />

2t 0<br />

where <strong>the</strong> current rises to a maximum I 0 in a time t 0 , at least for early times. Employing <strong>the</strong><br />

identity<br />

sin 4 z = 3 8 − 1 2 cos 2z + 1 8 cos 4z = z4 − 2 3 z6 + 1 5 z8 − 34<br />

445 z10 + 62<br />

14175 z12 ··· (4.17)<br />

and <strong>the</strong> dimensionless parameters, x = a(t)/a 0 , y = t/t 0 and<br />

α 2 = µ 0I0 2t 0<br />

2<br />

4πa0 2M (4.18)<br />

l<br />

a series solution <strong>of</strong> <strong>the</strong> form<br />

x = 1 − a 6 y 6 + a 8 y 8 − a 10 y 10 + a 12 y 12 ··· (4.19)<br />

can be found where a 6 = α 2 π 4 /480,a 8 = α 2 π 6 /5376 and a 10 = α 2 π 8 /115 200. The<br />

nonlinear effect <strong>of</strong> α 2 enters for higher order terms, e.g. a 12 = 17α 2 (π/2) 10 /62 370 −<br />

α 4 π 8 /1 013 760. This series converges only very slowly, if at all, for practical values <strong>of</strong> α 2 .<br />

Fur<strong>the</strong>rmore <strong>the</strong> current from a pulse-power generator is strongly affected by <strong>the</strong> impedance<br />

<strong>of</strong> <strong>the</strong> load especially due to strongly increasing inductance as <strong>the</strong> shell converges to <strong>the</strong> axis.<br />

Coupling <strong>the</strong> equation <strong>of</strong> motion to a circuit equation (as was done for example in [122])<br />

requires a numerical solution.<br />

However a new approach to obtain an exact, closed, analytic solution <strong>of</strong> equation (4.14)<br />

with a current waveform that peaks prior to final stagnation can be found as follows. For<br />

example, if <strong>the</strong> leading term in <strong>the</strong> above solution (equation (4.19)) is taken, i.e.<br />

a(t)<br />

= 1 − α2 π 4<br />

a 0 480<br />

( t<br />

t 0<br />

) 6<br />

(4.20)<br />

and substituted into equation (4.14) to give <strong>the</strong> current I(t)as<br />

( ) πt 2 (<br />

I(t) = I 0 1 − α2 π 4 t 6 ) 1/2<br />

2t 0 480 t0<br />

6 . (4.21)<br />

These values <strong>of</strong> a(t) and I(t)exactly satisfy equation (4.14). I has a maximum I m at t = t m<br />

given by<br />

( )<br />

t m<br />

= 121/6 2 2/3<br />

= 1.12 , (4.22)<br />

t 0 α 1/3 π α1/3 I m<br />

= 35/6 π 2/3 2.40<br />

= . (4.23)<br />

I 0 5 1/2 α2/3 α2/3 It follows that t m = t 0 for α = 1.40 while I m = I 0 for α = 3.71. A smaller value <strong>of</strong> M l a0<br />

2<br />

results in larger values <strong>of</strong> α and hence smaller values <strong>of</strong> t m and I m .<br />

To fur<strong>the</strong>r guide <strong>the</strong> choice <strong>of</strong> experimental parameters for a given generator (or vice<br />

versa) it is useful to consider <strong>the</strong> final stagnation. It is assumed to occur at a time t s when <strong>the</strong><br />

61

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