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Driver Calibration

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 $\mu$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 [*].



 
Table: Driver Characterization Shot List
Shot Press. Flow Duration Delay D1-2 D2-3 $\Delta$P1 $\Delta$P2 $\Delta$P3
  (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

1Pressure signals too small on CAMAC data; oscilloscope failed to trigger
2Driver did not detonate

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.

\begin{displaymath}\rm Injection~Period = 8.1513(Dial~Setting)-122.26 \end{displaymath}

and

\begin{displaymath}\rm Ignition~Delay = 3.5(Dial~Setting)+325 \end{displaymath}

where the injection period and ignition delay are in units of milliseconds.

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 $\gamma$, X, P0, and Ec, where Ec is the equivalent energy of the source:

\begin{displaymath}\frac{\Delta P}{P_0} = \frac{4\gamma/(\gamma+1)}{\sqrt{1+4\gamma/
(\gamma^2-1)\cdot X/L_e}-1} \end{displaymath}

where

\begin{displaymath}L_e = \frac{E_c}{P_0} \end{displaymath}

Far field is considered to be X/Le > 0.3.

Solving these relations for Ec in terms of $\gamma$, $\Delta P/P_0$, 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. [*].


  
Figure: Driver equivalent energy
\begin{figure}
\centering
\epsfig{file=tables/plot.ps, height=5.5in, angle=270}
\end{figure}

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.


next up previous contents
Next: Validation Figures Up: No Title Previous: Experimental Test Matrix
Joe E. Shepherd
2000-01-17