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A History of Research and a Review of Recent Developments

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References 69<br />

in Los Angeles Harbour, USA, at Christmas 1976, <strong>and</strong> in the Norwegian<br />

tanker King Haakon VII.<br />

3.5 THERMAL FLASH<br />

A final characteristic <strong>of</strong> explosions must be examined before we end this brief<br />

survey.<br />

Structural damage <strong>of</strong> a quite different nature can result from the extremely<br />

high temperatures created by the fireball <strong>of</strong> a nuclear explosion. The maximum<br />

fireball diameter for a 1 megaton bomb yield is about 1.4 miles, <strong>and</strong> for a 10<br />

megaton weapon it would be 3.4 miles. The thermal flash from bombs <strong>of</strong> this<br />

magnitude can cause changes to properties <strong>of</strong> materials, <strong>and</strong> can weaken the<br />

resistance <strong>of</strong> metal structures that contain material <strong>of</strong> relatively low melting<br />

point. It might well be that an aluminium alloy structure would be robust enough<br />

to withst<strong>and</strong> the shock pressures <strong>and</strong> blast winds from a large nuclear explosion,<br />

but be seriously weakened because <strong>of</strong> a reduction in pro<strong>of</strong> strength <strong>of</strong> the material.<br />

For a low yield nuclear explosion, heat pulses at a range <strong>of</strong> 1000ft from<br />

ground zero are <strong>of</strong> the order <strong>of</strong> 50 to 150 cals/cm 2 . A heat pulse <strong>of</strong> 1000 cals/<br />

cm 2 is about equivalent to a maximum surface temperature in structural<br />

aluminium <strong>of</strong> 250° C, <strong>and</strong> for aluminium plating between 0 <strong>and</strong> 0.5 inches<br />

thick, this will lead to a reduction in strength by annealing. If a heat pulse <strong>of</strong><br />

100 cal/ cm 2 is applied to the front face <strong>of</strong> a slab inch thick, the front <strong>and</strong> back<br />

faces will have both reached 250° C after 2 seconds. However, if the slab is<br />

inch thick, it has been shown by Parkes [3.20] that the behaviour is different.<br />

The front face, after reaching a maximum temperature <strong>of</strong> 200°C, falls gradually<br />

in temperature to reach a final value <strong>of</strong> 120°C after 2.5 seconds. Meanwhile the<br />

back face rises more gradually in temperature to reach the same final value.<br />

By analysing structural members as a number <strong>of</strong> laminations, each with<br />

varying strain <strong>and</strong> properties, Parkes showed that it is possible to estimate the<br />

residual stress distribution after a period <strong>of</strong> uneven cooling. A high residual<br />

tensile stress means that a subsequent tensile loading <strong>of</strong> the member will cause<br />

failure at a relatively lower applied stress. Care should therefore be taken to<br />

inspect apparently undamaged aluminium alloy structures after a nuclear<br />

explosion to check for minor deflection <strong>and</strong> distortions that signify a noticeable<br />

reduction in structural strength.<br />

3.6 REFERENCES<br />

3.1 Fletcher, R.F. (1968) Characteristics <strong>of</strong> liquid propellant explosions, Prevention<br />

<strong>and</strong> Protection against Accidental Explosion <strong>of</strong> Munitions, Fuels <strong>and</strong> Other<br />

Hazardous Mixtures, New York Academy <strong>of</strong> Sciences, 432.<br />

3.2 High, R.W. (1968) The saturn fireball, Prevention <strong>and</strong> Protection against<br />

Accidental Explosion <strong>of</strong> Munitions, Fuels <strong>and</strong> Other Hazardous Mixtures, New<br />

York Academy <strong>of</strong> Sciences, 441.

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