The driver of the GALCIT Detonation Tube is intended to reliably and controllably initiate detonations in any mixture that is detonable in the tube [Akbar and Shepherd (1996)]. It consists of acetylene and oxygen cylinders, regulators, flash arrestors, and valves, an injection valve, a digital control circuit, and an exploding wire circuit. The control circuit actuates the electropneumatic valves to control the driver injection duration and ignition delay, and triggers the exploding wire. It is interlocked to various gas supply valves and hydraulic closure devices for safety purposes.
A manual fire signal starts the driver sequence. The control circuit opens
the acetylene and oxygen valves and the injection valve for a programmed
time period and then waits for a programmed delay period. The ratio of
acetylene to oxygen is controlled by adjusting the cylinder pressure
regulators. A fire signal
is then sent to a trigger module that sends a high voltage trigger to
the exploding wire spark gap. The spark gap switches the 2 F
capacitor bank (typically charged to 9 kV) through a small copper wire
in the tube. The oxy-acetylene mixture is easily initiated by this
discharge and transitions to a planar detonation wave which is transmitted
to the test mixture.
Tests are periodically performed to verify the overall quantity of driver gas injected with each shot and to measure and adjust its equivalence ratio. To check the amount of gas injection, the driver is triggered several times without the exploding wire and the final pressure is measured after each injection. Measuring the detonation wave speed in this mixture and comparing it to equilibrium calculations (STANJAN) allow an estimate of the equivalence ratio. The driver is kept slightly lean to avoid formation of soot.
A number of tests with the driver transmitting blast waves into air have
been performed to evaluate its equivalent energy. A summary of results
from these shots is presented in Table .
Shot | Press. | Flow Duration | Delay | D1-2 | D2-3 | ![]() |
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(kPa) | (dial) | (s) | (dial) | (s) | (m/s) | (m/s) | (kPa) | (kPa) | (kPa) | |
48 | 100.0 | 560 | 4.442 | 200 | 1.025 | 712 | 658 | 430 | 330 | 270 |
581 | 100.08 | 560 | 4.442 | 200 | 1.025 | - | - | |||
59 | 25.2 | 560 | 4.442 | 200 | 1.025 | - | - | 361 | 210 | 150 |
60 | 25.2 | 560 | 4.442 | 200 | 1.025 | 999.5 | 846.7 | 305 | 206 | 163 |
61 | 50.2 | 560 | 4.442 | 200 | 1.025 | 823.6 | 739.1 | 340 | 224 | 185 |
62 | 75.2 | 560 | 4.442 | 200 | 1.025 | - | - | 434 | 312 | 253 |
63 | 100.0 | 560 | 4.442 | 200 | 1.025 | 711.8 | 652.1 | 350 | 270 | 230 |
642 | 98.9 | 69 | 0.440 | 200 | 1.025 | - | - | |||
65 | 99.69 | 260 | 1.997 | 200 | 1.025 | 453.5 | 450.7 | 95 | 90 | 80 |
662 | 99.47 | 137.7 | 1.000 | 200 | 1.025 | - | - | |||
67 | 100.0 | 751 | 6.000 | 200 | 1.025 | 744.8 | 683.2 | 500 | 330 | 310 |
68 | 100.0 | 628.5 | 5.000 | 200 | 1.025 | 716.8 | 663.3 | 450 | 340 | 290 |
69 | 100.0 | 505.8 | 4.000 | 200 | 1.025 | 689.3 | 635.3 | 430 | 280 | 240 |
70 | 100.0 | 383.1 | 3.000 | 200 | 1.025 | 655.2 | 599.5 | 350 | 230 | 200 |
71 | 100.0 | 560 | 4.442 | 200 | 1.025 | 705.7 | 644.4 | 420 | 300 | 240 |
72 | 100.0 | 560 | 4.442 | 50 | 0.500 | 706.6 | 651.9 | 500 | 330 | 270 |
73 | 100.0 | 560 | 4.442 | 336 | 1.501 | 707.9 | 645.3 | 400 | 280 | 250 |
74 | 100.0 | 560 | 4.442 | 479 | 2.002 | 696.1 | 646.6 | 510 | 380 | 280 |
75 | 100.0 | 560 | 4.442 | 765.1 | 3.003 | 701.1 | 646.4 | 350 | 270 | 240 |
The injection and delay periods are programmed through dial potentiometers.
The relationship between the numerical values on these potentiometers and
the actual injection and delay periods has been measured, and for reference are
given below.
According to the approximate analysis by [Thibault et al. (1987)], the
far field
overpressure in a tube subjected to a blast wave at X=0 is a function
of ,
X, P0, and Ec, where Ec is the equivalent energy
of the source:
Solving these relations for Ec in terms of ,
,
and X allows the data in Table
to be used to plot
equivalent energy vs injection time. These data, and a semilog curve
fit are shown in Fig.
.
Each point represents a shock pressure measured at one of the pressure transducers. The equivalent energy computed from the three transducers for each shot were averaged and used to calculate explosion lengths (Le) and the nondimensional distance to each transducer. Since the nondimensional distance to each transducer was a function of the initial pressure and the injection time, the validity of the far field assumption was checked for each pressure trace and the data points were sorted and plotted accordingly. The ``far field'' data were found to lie along a linear curve in linear-log coordinates, so a semilog curve fit was made and plotted with the data. The applicability of this fit is limited to the range of injection times investigated. Below about 2 s injection time the driver slug itself will not initiate. Above 6 s, the equivalent energy begins to plateau and the length of the driver slug begins to become appreciable (especially at low initial pressures). However, the data are useful by demonstrating that the relationship between equivalent energy and injection time is not linear. The effect of varying the delay time has also been investigated but no trend with respect to equivalent energy has been found.
Note that the analysis illustrated here assumes that certain system variables are constant, namely oxygen and acetylene delivery pressures and flow rates. These can be affected by variations in cylinder pressure and in the detonation tube initial pressure. Acetylene delivery pressure depends strongly on the frequency of use since the gas is dissolved in acetone within the cylinder. Furthermore, the specific construction of each cylinder can affect its flow characteristics. Variations in the component flow rates can affect the equivalence ratio and the driver equivalent energy. Efforts have been made to compensate for these variations, and tests are performed periodically to correct them.