Detonation wave
A detonation wave is a shock wave that spreads in all directions due to an explosion if the original expansion speed is greater than the speed of sound in the surrounding medium.
The prerequisite for rapid expansion is an increased sound speed of the exploding material, typically in connection with high temperatures . A steam boiler explosion leads to a detonation wave, while the bursting of a compressed air tank only leads to a bang.
General
'Quiet' sound waves obey the linear wave equation . Such sound waves can penetrate each other without interaction. The criteria for 'quiet' (regardless of the eardrum) are that both the sound pressure and the dynamic pressure due to the speed of sound are small compared to the static pressure . Immediately understandable reasons: The total pressure must not become negative and with the pressure rises and falls also the temperature and thus the speed of sound. Illustrative consequence: a short wave train riding a long wave crest runs faster than this until it reaches the front flank. An even shorter one is superimposed on the two, etc., so that the steepness of all the front flanks is added.
In 1946 Friedlander proposed the waveform shown opposite. For pressures that are not too high, it fits well to experimentally determined pressure curves. The following formula specifies this waveform as a pressure curve over time at a fixed point in space:
- for t > 0, otherwise
Description: Starting from the undisturbed, static pressure , the pressure jumps up instantaneously and then swings up with an undershoot (down ) .
In the area , the temperature can drop below the dew point and a Wilson cloud can form if the air humidity is sufficient and the distance from a possibly nuclear fireball is large enough.
For higher pressures, the temperature rises so high that the air is dissociated into atoms and ionized. Firstly, this changes the equation of state ; secondly, there is a lot of thermal radiation , which also contributes to the conduction of heat via the steep impact front to dissipate the energy in the wave. In nuclear explosions, the thermal radiation is in the UV and X-ray range, i.e. it is absorbed by air, which complicates the calculation of the detonation wave.
With the propagation, however, the energy is distributed over an ever larger surface of the shock front until the wave changes into a normal sound wave, which only propagates at the speed of sound.
A much more complex problem is the behavior of the pressure wave under reflection . An explosion in the vicinity of a flat, hard surface (e.g. the ground in an air explosion, Fig. 2) leads to an amplification of the pressure wave, which becomes maximum for different distances (detonation heights) from the reflecting surface at different pressure values. The ratio between the reflected pressure wave and the incident pressure wave is called the reflection factor. The typical non-linear behavior of shock waves during reflections was extensively investigated by the USA and the Soviet Union in aboveground nuclear weapons tests in the 1950s .
A mathematical model for atmospheric detonation waves
The former US Defense Nuclear Agency (DNA) developed a model for the computational estimation of explosion pressure waves around 1984, which provides the dependence of the overpressure peak as a function of the distance as well as the detonation height and the explosive energy. Although the model was originally developed for nuclear explosions , it can also be applied to almost any other explosion types using scaling rules, provided the explosion originates from a point source and inhomogeneities in the surrounding medium or the reflective surface are negligible. The model, which is available in the form of a DOS BLAST program , is not subject to confidentiality. It is based essentially on the Rankine-Hugoniot equation and empirical Ausgleichungsrechnungen on the basis of Nuclear test data on.
Effects
Pressure difference in mbar | Destructive effect |
---|---|
2 | Broken glass fewer windows that are already under tension |
3 | Glass breakage due to sound pressure of more than 140 dB |
30th | Slight damage to roofs; Glass breakage on 10% of the windows |
30-100 | Destruction of windows; first damage to window frames |
50 | Small damage to houses |
70 | Partial destruction of houses |
70-140 | Destruction of corrugated iron and wooden walls |
70 | Injuries from flying splinters |
90-500 | Damage to steel structures |
140 | Massive damage to houses and roofs |
140-200 | Brickwork collapse |
160 | Tympanic membrane rupture |
170 | Destruction of 50% of the brick houses |
200-280 | Destruction of steel frames |
350-500 | Almost complete destruction of buildings |
480 | Overturning cars |
480-550 | Failure of brick walls 20 to 30 cm thick |
620 | Destruction of cars |
700 | Complete destruction of buildings |
The Tsar bomb caused the largest artificial shock wave.
See also
literature
- GF Kinney, KJ Graham: Explosive shocks in air. Springer, Berlin / New York 1985, ISBN 3-540-15147-8 .
- Arnold Berliner, Karl Scheel (Hrsg.): Physical hand dictionary. Second edition, published by Julius Springer, Berlin 1932.
- Wilhelm Jost: Explosion and combustion processes in gases. Published by Julius Springer, Berlin 1939.
Web links
- BLAST program and others
- Detonation waves in narrow crevices (accessed February 13, 2020)
- Heat transformation processes without phase transformation (accessed on February 14, 2020)
- Efficient numerical simulation of the deflagration-detonation transition (accessed on February 14, 2020)
- On the detonation physics of solid and liquid explosives (accessed on February 14, 2020)
Individual evidence
- ^ JM Dewey: The shape of the blast wave: studies of the Friedlander equation. Presented at the 21st International Symposium on Military Aspects of Blast and Shock, Israel 2010 ( Online ).
- ↑ PDF at www.nrc.gov .