| Chapter 7 | |
Blast Waves |
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If a strong gas explosion occurs inside a process area or in a compartment,
the surrounding area will be subjected to blast waves. The magnitude of
the blast wave will depend on:

| Figure 7.1. | Free field blast wave. |
Figure 7.2 shows maximum explosion overpressures from various CMR experiments
in a 50 m3 tube, a wedge-shaped vessel (results scaled to 50
m3) and a 50 m3 offshore module, together with the
associated blast wave overpressure variation with distance. The horizontal
part of the curves indicate the extent of the gas clouds before the explosions
(actually the radius of a hemispherical cloud of the same volume as the
experiment). No legend discriminating between the explosion vessels is
given, since the gas volume and explosion overpressure are the important
parameters here.

| Figure 7.2. | Peak pressure from free field blast for CMR experiments in 50 m3 test vessels. (Hjertager et al., 1981, Bjerketvedt and Bjørkhaug, 1991) |
The results show that the blast wave from a gas explosion can cause
high pressures far away from the area where the explosion actually takes
place. In safety evaluation, free field blast must therefore be considered.
In accident investigations evaluation of the free field blast from recorded
damage is often used for evaluation of the source strength of the explosion.
The objective of this chapter is:
i) To describe the nature of a blast wave from a gas explosion.
ii) To present methods to estimate the blast waves from a gas explosion.
The blasts from detonations of high explosive charges, such as TNT, are fairly well documented. (Baker et al., 1983). The peak explosion pressure for blast waves from TNT explosions with charges ranging from 1 kg to 1000 kg, as function of distance R (from the centre of the charge) is shown in Figure 7.3.

| Figure 7.3. | Peak explosion pressure (side-on) vs. distance for TNT ground burst. |
These data can be scaled through a normalised length scale (Hopkinson
scaling) R*
| R* = R/W1/3 | (7.1) |
where R [m] is the distance from the centre of the explosive source
and W[kg] is the mass of the explosive source. Figure 7.4 shows the same
set of data as shown in Figure 7.3, but plotted versus the normalised length
scale R*.
Similar diagrams as Figure 7.4 also exist for duration, impulse and
other blast parameters. These curves can be found in Baker et al. (1983).

| Figure 7.4. | Peak explosion pressure (side-on) versus scaled distance, R*, for TNT ground burst. |
The diagram for TNT detonations have been used for estimations of blasts
from gas explosions, even though there are differences between the blasts
from a gas explosion and a TNT-detonation (Shepherd et al., 1991, van den
Berg, 1985). In a gas explosion the local pressure may reach values as
high as a few bars. The blast pressure for TNT explosions is much higher
close to the charge. Such near-field data are therefore irrelevant for
gas explosions and it is recommended not to use TNT-data indicating pressures
higher than 1 bar to estimate gas explosion blasts.
The so-called TNT equivalence method has been widely used for gas explosions.
The TNT equivalence method applies pressure-distance curves for TNT explosions
to gas explosions and the equivalent TNT charge is estimated from the energy
content in the exploding gas cloud.
For typical hydrocarbons, such as methane, propane, butane etc., the
heat of combustion is 10 times higher than the heat of reaction of TNT.
The relation between the mass of hydrocarbons WHC and the equivalent
TNT charge WTNT is then
| WTNT » 10 * h * WHC | (7.2) |
where h is a yield factor (h
= 3%-5%), based on experience, see Gugan, 1978.
In the original TNT equivalence method, the mass of hydrocarbon WHC
was based on the total mass released and the yield factor h.
In order to estimate consequences of gas explosions, the geometrical conditions
(i.e. confinement and obstructions) have to be taken into account. In the
original TNT equivalence method, the geometrical conditions are not taken
into account. The results from this type of analysis have therefore hardly
any relevance and should in general not be used.
The drawbacks of the TNT equivalence method can be listed as follows:
In order to take the geometrical effects into account in the TNT equivalence
method, Harris and Wickens (1989) proposed to use a yield factor of 20%
(h = 0.2) and the mass of hydrocarbon, WHC,
contained in Stoichiometric proportions in any severely congested region
of the plant. For natural gas the equivalent mass of TNT can be estimated
from (assuming atmospheric pressure initially)
| WTNT » 0.16V [kg] | (7.3) |
where V [m3] is the smaller of either the total volume of
the congested region or the volume of the gas cloud. Equation 7.3 will
also hold for most hydrocarbons, since the energy content per volume Stoichiometric
mixture is approximately the same (~3.5MJ/m3).
Figure 7.5 shows the results from a TNT equivalent analysis, as suggested
by Harris and Wickens, in comparison with CMR's experimental results from
50 m3 tests.

| Figure 7.5. | Peak explosion pressure (side-on) versus distance for TNT equivalence
method |
As we can see from this figure there is fairly good agreement between
the predicted values and the experimental values as long as the explosion
pressure in the cloud is in a few bars range. Weak gas explosions (less
than 0.5 bar) are not represented satisfactorily. This indicates that the
TNT equivalence method can be useful as a rough approximation if one uses
a yield factor of 20% and appropriate values for WHC or V. However,
for explosion pressures below 1 bar, the TNT equivalence method will overestimate
the blast. More sophisticated methods must therefore be applied for such
cases.
The multi-energy method (van den Berg, 1985) is a more sophisticated
method than the TNT-equivalence method. It can estimate the blast from
gas explosions with variable strength. The method is based on numerical
simulation of a blast wave from a centrally ignited spherical cloud with
constant velocity flames. By varying the flame velocity, a set of curves
for different explosion strengths (i.e. explosion pressure inside the cloud)
have been produced. Figure 7.6 shows the dimensionless curves that are
used in the multi-energy method.

| Figure 7.6. | Hemispherical fuel-air charge blast for the multi-energy. |
Figure 7.6 is in principle the same figure as the previous blast curves
for TNT. For a detonating cloud, curve 10 can be used. For a deflagration
(curves 1 to 9) we see that the pressure profile inside the cloud is not
a shock wave followed by an expansion wave, but it can either be a shock
wave followed by increasing pressure that drops off after the passage of
the flame front or a sonic wave (i.e. gradually increasing pressure) that
drops after the flame front.
However, as a blast propagates away from the centre of the explosion,
the gradient at the front will steepen and eventually become a shock wave,
like the blast from a TNT charge.
The difficult part of a multi-energy method analysis is to choose:
i) The explosion pressure within the exploding gas cloud (i.e. the charge
strength
ii) The combustion energy, E, given the size of the gas cloud contributing
to the blast (i.e. the charge size).
The multi-energy method does not give any information about which explosion
pressure (charge strength) to choose in a blast analysis. That information
has to be found separately by using numerical simulations, experimental
data or make a conservative assumption. The combustion energy, E, is also
a parameter that is not straightforward to estimate.
For a Stoichiometric hydrocarbon-air mixture of volume V, the combustion
energy E can be estimated from
| E » 3.5 (MJ/m3) * V | (7.4) |
In an accidental explosion (deflagration), only the confined and/or
congested areas will contribute to blast generation. Therefore only portions
of the total cloud volume should be included in equation (7.4). Van den
Berg (1985) indicates that the total volume of a confined and/or congested
area should be used in equation (7.4). However, even such an approach can
lead to conservative numbers and overestimate the blast in some situations.
For instance in an explosion in a partly confined volume, the total volume
will give conservative data, particularly in low pressure cases. During
the explosion as the gas cloud burns the gas will expand and push the unburned
gas outside the confinement. The gas that is pushed outside the confinement,
will often not contribute significantly to the generation of the blast.
Before we leave the multi-energy method there is one aspect of gas explosions
that is discussed by van den Berg (1985) which should be mentioned. In
a process area for instance, one large gas cloud can cause multiple blast
waves. To illustrate this we include Figure 7.7. In this Figure we can
see that the gas cloud covers two obstructed areas. Between these areas
there is open space. If we assume that the cloud ignites in area A, we
will first get an explosion in area A. If no transition to detonations
occurs in area A, the flame velocity will drop when the flame propagates
outside area A. In an open area, the flame velocity will be so slow that
the pressure generation will be negligible. When the flame reaches area
B, the flame will accelerate again and a new blast wave will be generated.
If one monitors the pressure at location C, one will observe two blast
waves passing.

| Figure 7.7. | One gas cloud may cause more than one blast wave. |
This feature was also confirmed experimentally. Explosion propagation
from one obstructed area into a second nearby obstructed area at various
intervening distances shows deceleration of the flame upon propagating
outside the first obstructed area and a re-acceleration within the second
obstructed area (Figure 7.8) (van Wingerden, 1989).

| Figure 7.8. | Explosion propagation in two obstructed areas with an intervening area filled with gas in between them. Both obstructed areas have a length of 2 m. The length of the intervening area (S) was varied between 0.5 m and 2 m (van Wingerden, 1989). |
An alternative to the TNT-equivalence method and the multi-energy method
is to scale experimental results. In Figure 7.2
some data from CMR experiments were presented. Based on these data and
by applying scaling with dimensionless length scale, a set of curves for
explosions with different strengths, for a 1000 m3
compartment, have been developed. The curves are shown in Figure 7.9.

| Figure 7.9. | Peak explosion pressure for blast waves from explosions in a 1000 m3 confinement. |

| Figure 7.10. | Peak explosion pressure for blast waves from 1 barg explosions in a 100, 1000, 10,000 and 100,000 m3 confinement. |
For an explosion in a confinement of volume V the blast wave can be
found simply by scaling the actual distance from the explosion centre R
to an equivalent distance REq1000 and use that distance in Figure
7.9.
![]() |
(7.5) |
Results from such scaling are shown in Figure 7.10.
Several advanced numerical codes for blast prediction exist. However,
all these types of codes have limitations. They need either a predefined
flame speed or explosion pressure (i.e. they cannot estimate source term)
or they require computers of an order of magnitude larger than we have
today to handle both flame propagation and blast propagation.
Savvides and Tam (1991) have compared FLACS results with results from
TNT equivalence and multi-energy methods. It was found that in the test
cases used, the high overpressure was created in localised pockets within
the plant, where the density of equipment was high. They observed that
the overpressure decayed rapidly in open space. The conclusions were that
a numerical simulation model like FLACS provides much more information
than the simpler models, but the requirement for computer time is high
for process plants. They foresee that such simulations will become a routine
task in assessing explosion hazards.
At CMR the FLACS-3D code has been used for combined explosion and blast
simulations even though the main use of FLACS is in simulating gas explosions
only. The main difference between the two applications is that blast simulations
are usually performed on a large calculation domain, where the explosion
takes place in a smaller part of this domain. Due to limitations in computer
capacity larger control volumes must be used, which may not be compatible
with the fact that in onshore plants localised explosions can be very important.
To handle localised explosion in the simulations, small control volumes
are needed. However, for local explosions of a given source strength, FLACS
is still suited to predict blast decay in congested or semi-confined surroundings
of the exploding gas cloud.
Figures 7.10 and 7.11 compare examples of blast decay simulations using
FLACS in local explosions in a process plant with scaled experimental results
(using equation 7.5) for two clouds of 20 m3 and 600 m3
respectively. The scaled experimental results are based on one test in
CMR's 50 m3 model of an offshore module (Figure 7.11 only, see
section 5.6) and on two tests in the
10 m long tube (see section 5.3),
producing maximum pressures inside the gas cloud of 0.2, 1 and 6 barg respectively.
The FLACS simulations generate 0.3 bar overpressure in the 20 m3
cloud and 5-6 bar overpressure in the 600 m3 cloud. The simulated
pressure decay outside the gas clouds shows a behaviour very similar to
the experimental results. The observed deviations may be due to differences
in congestion outside the exploding gas cloud.

| Figure 7.11. | Blast decay for a 20 m3 gas cloud. FLACS simulations versus scaled experiments. |

| Figure 7.12. | Blast decay for a 600 m3 gas cloud. FLACS simulations versus scaled experiments. |
The vertical lines in Figures 7.11 and 7.12 show the radius of equivalent,
hemispherical gas clouds of volumes 20 m3 and 600 m3
respectively.
7.6 Reflection of Free Field Blast Waves
The loading on a construction hit by a blast wave is a rather complex
phenomenon. (Baker et al.(1983).
When a free field blast wave runs into an object like a building, the
wave will be reflected. Figure 7.13 shows how a shock wave is reflected
off a building. Due to reflection and diffraction, the wave loading on
the walls and the roof will differ. The maximum loading will be on the
wall facing the explosion. At this wall the shock wave will be reflected
and the pressure will typically increase by a factor of 2. (Depends on
shock strength.).
When the shock wave propagates in a free field, the gas behind the shock
wave will have a velocity in the same direction as the wave propagates.
When the shock wave hits the wall, the gas must stop and the dynamic pressure
(i.e. 0.5 ru2) is transformed to
pressure. This is in principle why the pressure increases due to blast
wave reflection.
On the opposite wall (see Figure 7.13) the shock wave will be diffracted,
and that will reduce the pressure load on the building.

| Figure 7.13. | Blast reflection off a building. |
7.7 Guidelines for Blast Waves
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