MEASUREMENTS OF UNDERWATER EXPLOSION PERFORMANCES BY PRESSURE GAUGE USING FLUOROPOLYMER

Similar documents
An underwater explosion is an explosion where the point of detonation is below the surface of the water.

Study on Intensity of Blast Wave Generated from Vessel Bursting by Gas Explosion

Offshore platforms survivability to underwater explosions: part I

Old-Exam.Questions-Ch-14 T072 T071

Development of a Shock Loading Simulation Facility

Development of High-speed Gas Dissolution Device

. In an elevator accelerating upward (A) both the elevator accelerating upward (B) the first is equations are valid

Unit 2 Kinetic Theory, Heat, and Thermodynamics: 2.A.1 Problems Temperature and Heat Sections of your book.

PHYS 101 Previous Exam Problems

[2] After a certain time, the temperature of the water has decreased to below room temperature.

Seismic Sources. Seismic sources. Recorders. Requirements; Principles; Onshore, offshore. Digitals recorders; Analog-to-Digital (A/D) converters.

AP Physics B Ch 10 Fluids. MULTIPLE CHOICE. Choose the one alternative that best completes the statement or answers the question.

Irrigation &Hydraulics Department lb / ft to kg/lit.

DYNAMIC CRUSH TEST ON HYDROGEN PRESSURIZED CYLINDER

1. The principle of fluid pressure that is used in hydraulic brakes or lifts is that:

FROTH: Fundamentals and Reliability of Offshore Structure Hydrodynamics EPSRC

CHARACTERISTICS OF LEAK DETECTION BASED ON DIFERENTIAL PRESSURE MEASUREMENT

MODEL OF IMPACT UNDERWATER DETONATION

Third measurement MEASUREMENT OF PRESSURE

Static Fluids. **All simulations and videos required for this package can be found on my website, here:

The water supply for a hydroelectric plant is a reservoir with a large surface area. An outlet pipe takes the water to a turbine.

INFLUENCE OF INITIAL PRESSURE ON THE IGNITION AND COMBUSTION OF A PROPELLING CHARGE. Patrice Franco

Lecture 19 Fluids: density, pressure, Pascal s principle and Buoyancy.

MS.RAJA ELGADY/PRESSURE PAPER 3

ARA PROJECT Prepared by: Peter T. Dzwilewski Applied Research Associates, Inc Shaffer Parkway Littleton, Colorado 80127

Student name: + is valid for C =. The vorticity

Fall 2004 Homework Problem Set 9 Due Wednesday, November 24, at start of class

Slide 5 / What is the difference between the pressure on the bottom of a pool and the pressure on the water surface? A ρgh B ρg/h C ρ/gh D gh/ρ

Chapter 9 Solids and Fluids

End of Chapter Exercises

Application of Simulation Technology to Mitsubishi Air Lubrication System

MODELLING OF FUME EXTRACTORS C. R.

Fig. 2. M.I. Yaroslavtsev, 2002

Vacuum P=0. h=76 cm A B C. Barometer

WATER HYDRAULIC HIGH SPEED SOLENOID VALVE AND ITS APPLICATION

Flow and Mixing in the Liquid between Bubbles

and its weight (in newtons) when located on a planet with an acceleration of gravity equal to 4.0 ft/s 2.

EXPERIMENTAL STUDY ON THE HYDRODYNAMIC BEHAVIORS OF TWO CONCENTRIC CYLINDERS

Chs. 16 and 17 Mechanical Waves

MEASURING UNDERWATER EXPLOSIONS: TRANSDUCERS AND THEIR APPLICATION

2 Available: 1390/08/02 Date of returning: 1390/08/17 1. A suction cup is used to support a plate of weight as shown in below Figure. For the conditio

Flow in a shock tube

Physics 221, March 1. Key Concepts: Density and pressure Buoyancy Pumps and siphons Surface tension

Dynamics of bubble rising at small Reynolds numbers

Energy and mass transfer in gas-liquid reactors.

Application Worksheet

Figure 1 Schematic of opposing air bearing concept

ASSIGNMENT 2 CHE 3473

ASSIGNMENT 2 CHE 3473

AP TOPIC 6: Gases. Revised August General properties and kinetic theory

A New Way to Handle Changing Fluid Viscosity and the Full-to-empty Effect

Experiment 8: Minor Losses

Pressure Measurement

Chapter 10: Gases. Characteristics of Gases

Engineering Flettner Rotors to Increase Propulsion

The Estimation Of Compressor Performance Using A Theoretical Analysis Of The Gas Flow Through the Muffler Combined With Valve Motion

1 SE/P-02. Experimental and Analytical Studies on Thermal-Hydraulic Performance of a Vacuum Vessel Pressure Suppression System in ITER

Numerical study of water plume behavior under shallow depth explosion

PHYSICS - CLUTCH CH 17: FLUID MECHANICS.

3. A fluid is forced through a pipe of changing cross section as shown. In which section would the pressure of the fluid be a minimum?

THERMODYNAMICS, HEAT AND MASS TRANSFER TUTORIAL NO: 1 (SPECIFIC VOLUME, PRESSURE AND TEMPERATURE)

Chapter 9 Fluids and Buoyant Force

INSTRUMENTS A THERMAL MASS FLOW SENSOR USING A CONSTANT DIFFERENTIAL TEMPERATURE ABOVE THE AMBIENT GAS TEMPERATURE

Final Report. Prepared By: Alexander G. Soloway Dept. of Mechanical Engineering, University of Washington, Seattle, Washington.

doi: /s

Chapter 10 Fluids. Which has a greater density? Ch 10: Problem 5. Ch 10: Problem Phases of Matter Density and Specific Gravity

Influence of rounding corners on unsteady flow and heat transfer around a square cylinder

Waves. harmonic wave wave equation one dimensional wave equation principle of wave fronts plane waves law of reflection

Applications of Bernoulli s principle. Principle states that areas with faster moving fluids will experience less pressure

Reactor Networks. D. G. Goodwin Division of Engineering and Applied Science California Institute of Technology. Cantera Workshop July 25, 2004

Analysis of Pressure Rise During Internal Arc Faults in Switchgear

Name Chemistry Pre-AP

1. All fluids are: A. gases B. liquids C. gases or liquids D. non-metallic E. transparent ans: C

AP B Fluids Practice Problems. Multiple Choice. Slide 2 / 43. Slide 1 / 43. Slide 4 / 43. Slide 3 / 43. Slide 6 / 43. Slide 5 / 43

12 fa. eel), Ara, Fl eat Mobi eu) r V14,:srholki CV -65 P- 1 1). e2r 46. ve, lactogin. 1 V eil - ( - t Teo. c 1 4 d 4. .'=- tit/ (4 nit) 6 --)

Chapter 10. When atmospheric pressure increases, what happens to the absolute pressure at the bottom of a pool?

CubeSat Balloon Drag Devices: Meeting the 25-Year De-Orbit Requirement

WAVE LOAD ACTING ON HORIZONTAL PLATE DUE TO BORE

CHAPTER 31 IDEAL GAS LAWS

Hydrostatics Physics Lab XI

AUDIO-VISUAL AND HYDROACOUSTIC OBSERVATIONS OF THE DEAD SEA CALIBRATION EXPERIMENT. Yefim Gitterman and Avi Shapira. Geophysical Institute of Israel

Detecting sound wave of bubbles produced in a boiling liquid

Problems of Chapter 3

HW-1: Due by 5:00 pm EDT on Wednesday 13 June 2018 to GradeScope.

End of Chapter Exercises

Classes at: - Topic: Gaseous State

The Performance of Vertical Tunnel Thrusters on an Autonomous Underwater Vehicle Operating Near the Free Surface in Waves

Experimental Verification of Integrated Pressure Suppression Systems in Fusion Reactors at In-Vessel Loss-of -Coolant Events

Properties of Fluids SPH4C

Precision level sensing with low-pressure module MS

ANSWERS TO QUESTIONS IN THE NOTES AUTUMN 2018

Science 8 Chapter 9 Section 1

3 1 PRESSURE. This is illustrated in Fig. 3 3.

Transverse waves cause particles to vibrate perpendicularly to the direction of the wave's motion (e.g. waves on a string, ripples on a pond).

Vapour pressure of liquids SURFACE TENSION

The Effect of Refrigerant Dissolved in Oil on Journal Bearings Reliability

Yasuyuki Hirose 1. Abstract

Variation in Pressure in Liquid-Filled Plastic Film Bags Subjected to Drop Impact

Chapter 13 Fluids. Copyright 2009 Pearson Education, Inc.

A numerical Euler-Lagrange method for bubble tower CO2 dissolution modeling

Transcription:

MEASUREMENTS OF UNDERWATER EXPLOSION PERFORMANCES BY PRESSURE GAUGE USING FLUOROPOLYMER Kenji MURATA, Katsuhiko TAKAHASHI, Yukio KATO* NOF Corporation 61-1 Kitakomatsudani, Taketoyo-cho, Chita-gun, Aichi 470-2398, JAPAN Pressure gauge using fluoropolymer as sensing element was developed to measure underwater shock wave profile at the location very close to the explosive-water boundary. Shock wave profile was successfully measured in high pressure range where peak shock wave pressure exceeded 400MPa for emulsion explosives and aluminized emulsion explosives. First bubble pulse profile was also precisely measured by pressure gauge using fluoropolymer. The experimental results shows that the late energy release by aluminum reaction in detonation products enhanced both shock wave and first bubble pulse. It is demonstrated that the impulse of first bubble pulse is about 2.5 times greater than shock wave impulse, although peak pressure of first bubble pulse is only 10~15% of peak shock wave pressure. INTRODUCTION During last decades, the underwater explosion test has contributed appreciably to understand the detonation effects of explosives in terms of their measured underwater shock and bubble effects 1,2. The underwater explosion test has some advantages over other experimental techniques such as pressure measurements, particle velocity measurements and cylinder test, because large mass of surrounding water provides sufficient confinement to maintain detonation products at high pressure, and allows to observe the state of detonation products at different pressure and time range. Particularly, in the case of aluminized explosives, sufficient confinement realized in the underwater explosion test enables relatively slow aluminum reaction to complete in detonation products. In the engineering applications such as shock forming of metal plates and shock consolidation of metallic and ceramic powders etc, the measurements of underwater shock wave in high pressure range are required to control shock wave loading on target samples. To understand destructive effects of underwater explosion phenomena, it is also important to measure precisely bubble pulse as well as shock wave. Underwater shock wave and bubble pulse have been widely measured by pressure gauge using tourmaline crystal. However, maximum measurable pressure is limited to pressure lower than 100 MPa, because tourmaline crystal is destroyed by high pressure generated due to the impedance mismatch with water. Pressure gauge using fluoropolymer has potentially the possibility to measure high underwater shock pressure (> 100 MPa), since shock impedance of fluoropolymer is very close to that of water. In our previous studies 3,4, we developed a pressure gauge using --------------------------------------------------------------------------------------------------------------- *Guest Professor of Shock Wave and Condensed Matter Research Center, Kumamoto University

fluoroplymer as sensing element, which can measure underwater shock wave pressure higher than 100 MPa. In the measurements of bubble phenomena by tourmaline gauge, a shift in bubble pulse base line to negative pressure after the passage of shock wave is observed. This deviation of bubble pulse base line to negative pressure makes the precise quantitative measurements of bubble pulse difficult. It is demonstrated that pressure gauge using fluoropolymer can maintain base line of bubble pulse after the passage of shock wave, and permits precise measurements of bubble pulse 5. In this study, underwater shock wave and bubble pulse were measured by pressure gauge using fluoropolymer for the emulsion explosives (EMX) and aluminized emulsion explosives (AL-EMX). It was demonstrated that pressure gauge using fluoropolymer can measure underwater shock wave profile in the pressure range higher than 400 MPa. Peak pressure and impulse of first bubble pulse were precisely measured and compared with those of shock wave. It was shown that aluminum reaction enhanced shock wave energy, shock wave impulse, first bubble impulse and bubble energy. EXPERIMENTAL Properties of sample explosives EMX and AL-EMX are shown in Table 1. Composition of base emulsion matrix 8m R A B (a) Experimental arrangements 36m 4m A 10m (b) Underwater explosion testing tank FIGUER 1. EXPERIMENTAL SET-UP (A) Charge, (B) Sensors, (R) Stand off distance B was consisted of 74.6wt% of ammonium nitrate, 10.6wt% of hydrazine nitrate, 10.6wt% of water, 4.2wt% of wax and emulsifier. Formed polystyrene sphere was used as micro-balloon. Aluminum powder was atomized type whose mean diameter was about 30µm. Figure 1 presents experimental set-up. The underwater explosion tests were performed in testing tank of 36m in diameter and 8m in depth. Sample explosive was set at the center of testing tank at depth of 4m, and pressure gauge was also set at depth of 4m. Distance between sample explosive and pressure gauge (R) was varied in wide range from 0.05 to 3m, and charge weight (W) was fixed to be 0.1kg. Consequently, scaled distance (R/W 1/3 ) was varied from 0.11 to 6.46m/kg 1/3. Sample explosive was formed in spherical shape whose radius was about 2.7cm, and centrally initiated by No.6 electric detonator. Figure 2 shows the structure of pressure gauge using fluoropolymer as sensing element. Size of fluoropolymer sensing element was 5mm square and 50µm thick. The pressure gauge was filled with insulation oil whose shock impedance was very close to that of water. The pressure gauge was connected to digital oscilloscope through buffer amplifier. Shock wave profile was recorded by digital storage oscilloscope (Nicolet model 460, sampling time 0.2µs), and bubble pulse was recorded by digital storage oscilloscope (Nicolet model Pro90, sampling time 20µs). D E A B C G FIGURE 2. STRUCTURE OF PRESSURE GAUGE (A) Sensing element (B) Body (C) Coaxial cable (D) Insulation oil (E) Cap (F) Metal tube (G) Insulation resin F

Sample explosive Table 1 Properties of sample explosives Density Detonation Composition velocity Base emulsion GMB Al powder ( g / cm 3 ) ( m /s ) ( wt % ) ( wt % ) ( wt % ) EMX 1.15 3390 98.9 1.1 0 AL-EMX 1.22 3360 82.4 0.92 16.7 Shock wave impulse (Is), shock wave energy flux density (EFDs), shock wave energy (Es), and bubble energy (Eb) were determined by following equations, using measured shock wave profile and bubble pulse profile; Is = 5θ 0 P( t) dt L (1) 1 EFDs = ρw Cw 4πR Es = W 2 5θ 0 EFDs L (3) Eb = 6.84 10 Po 5/ 2 P( t) Tb Here, ρw is density of water, Cw is sound velocity of water, θ is characteristic time of shock wave, P(t) is shock wave pressure at time t, Po is total hydrostatic pressure at charge depth and Tb is bubble period. RESULTS AND DISCUSSION The experimental conditions and results are summarized in Table 2. Underwater shock wave profile was successfully measured even in the condition that peak shock wave pressure exceeded 400MPa. In the case of EMX, measured shock wave energy decreases with the increase of scaled distance in the scaled distance range smaller than 0.3m/kg 1/3. It is well known that measured bubble energy is an invariant and independent of location of pressure gauge, but this is not true for shock wave energy. During shock wave transmission 3 2 dt L (2) / W L (4) from the explosive-water boundary to the pressure gauge, one part of shock wave energy is lost by shock heating of surrounding water. When shock wave pressure is higher, loss of shock wave energy is greater. According to the results of previous work 6,7,8, shock wave velocity decays to sound velocity of water, and loss of shock wave energy becomes negligible small at the distance of about 10 charge radii, that is about 0.3m in our experiments. However, in the case of AL-EMX, measured shock wave energy remains constant within the measured scaled distant range. This fact indicates that loss of shock wave energy during shock wave transmission is compensated by shock wave enhancement owing to the late energy release by aluminum reaction in detonation products. Figure 3 and 4 present typical shock wave profile for EMX and AL-EMX. Pressure decay in shock wave profile of AL-EMX is much slower than that of EMX, and shock wave characteristic time of AL-EMX is much longer than that of EMX owing to the effects of late energy release by aluminum reaction in detonation products. The effects of aluminum reaction on shock wave profile becomes more clear when peak shock wave pressure is higher. When pressure gauge is located very close to the explosive-water boundary, gas bubble of detonation products can arrive at the pressure gauge within observation time. In the case 1 and 11 where pressure gauge is located only about 2.5cm from the explosive-water boundary, gas bubble arrives the pressure gauge in less than 50µs after passage of shock wave, and then

pressure gauge can measure pressure of detonation products. Figure 5,6,7 present the relations between peak shock wave pressure (Pmaxs), scaled shock wave impulse (Is/W 1/3 ), scaled shock wave energy flux density (EFDs/W 1/3 ) and scaled distance. These relations can be expressed by similitude equations 2, and similitude constants and coefficients for EMX and AL-EMX are summarized in Table 3. Peak shock wave pressure of AL-EMX is slightly lower than that of EMX at scaled distance smaller than 1m/W 1/3, and becomes slightly higher than that of EMX at scaled distance larger than 1m/W 1/3 (Figure 5). Scaled shock wave impulse of AL-EMX is about 25% greater than that of EMX (Figure 6), and scaled shock wave energy flux density of AL-EMX is about 15% greater than that of EMX (Figure 7) within measured scaled distance range. Table 2 Experimental conditions and results Scaled distance Pmaxs EFDs Is Es Pmaxb Ib Case Sample Stand off distance R/W 1/3 ( Pa ( MJ/k ( Pa Explosive (m) (m kg 1/3 ) (m kpa) s) g) s) (MPa) (MPa) 1 0.05 0.11 464.6 2940.0 21099 0.924 46.4 80840 2 0.10 0.22 213.4 723.9 9999 0.910 20.6 37713 3 0.15 0.32 138.7 325.5 7975 0.920 15.7 24143 4 0.20 0.43 100.1 180.2 5207 0.906 9.6 17594 5 0.30 0.65 57.8 72.8 3692 0.823 7.4 11263 EMX 6 0.40 0.86 47.2 40.7 3082 0.818 5.7 8208 7 0.50 1.08 32.0 27.4 2643 0.861 4.1 6421 8 1.00 2.15 17.2 7.1 1351 0.887 2.1 2996 9 2.00 4.31 8.0 1.8 724 0.880 1.0 1398 10 3.00 6.46 5.1 0.8 503 0.866 0.7 895 11 0.05 0.11 383.5 3102.5 27879 0.975 58.0 90927 12 0.10 0.22 178.5 824.9 13815 1.037 29.4 43430 13 0.15 0.32 121.8 350.2 9665 0.990 19.1 28189 14 0.20 0.43 90.3 198.0 7396 0.995 13.5 20744 15 0.30 0.65 59.2 88.8 5073 1.004 8.1 13464 AL-EMX 16 0.40 0.86 43.9 50.2 3882 1.009 5.9 9908 17 0.50 1.08 34.8 32.3 3154 1.015 4.7 7811 18 1.00 2.15 16.9 8.2 1656 1.030 2.5 3731 19 2.00 4.31 8.2 2.1 869 1.056 1.4 1782 20 3.00 6.46 5.4 0.9 596 1.018 0.9 1157

FIGURE 3. EXAMPLE OF SHOCK WAVE PLOFILE FIGURE 4. EXAMPLE OF SHOCK WAVE PLOFILE FIGURE 5. RELATION BETWEEN PEAK SHOCK WAVE PRESSURE AND SCALED DISTANCE FIGURE 6. RELATION BETWEEN SCALED SHOCK WAVE IMPULSE AND SCALED DISTANCE

FIGURE 7. RELATION BETWEEN SCALED SHOCK ENERGY FLUX DENCITY AND SCALED DISTANCE Figure 8 shows the examples of bubble pulse profile measured by pressure gauge using tourmaline and fluoropolymer as sensing element. Bubble pulse profile measured by pressure gauge using tourmaline presents important shift in base line to negative pressure after the passage of shock wave, which makes the precise quantitative measurements of bubble pulse pressure and impulse difficult. In contrast, bubble pulse profile measured by pressure gauge using fluoropolymer maintains base line after the passage of shock wave. Figure 9 shows the enlargement of first bubble pulse profile. The duration of first bubble pulse is in the order of 10ms in the measured experimental conditions, and pressure rise is very slow compared with shock wave. Peak pressure of first bubble pulse was determined directly using measured bubble pulse profile. Bubble pulse impulse (Ib) was calculated using measured bubble pulse profile Pb(t) according to following equation; Ib = T 2 T1 P( t) dt L (5) Here, T1 and T2 are respectively the time when bubble pressure increases and decreases to threshold pressure P1. The threshold pressure P1 was selected as 5% of peak bubble pulse pressure considering noise level of measurements. The experimental results are summarized in Table 2. Figure 10 and 11 present the relations between peak bubble pulse pressure (Pmaxb), scaled bubble pulse impulse (Ib/W 1/3 ) and scaled distance. These relations can be expressed by similitude equations, and similitude constants and coefficients for EMX and AL-EMX are summarized in Table 3. Peak bubble pulse pressure of AL-EMX is about 25% higher than that of EMX, and scaled bubble pulse impulse of AL-EMX is about 20% greater than that of EMX within measured scaled distance range. The experimental results also show that the impulse of first bubble pulse is about 2.5 times greater than shock wave impulse within measured scaled distance range, although peak bubble pulse pressure is only 10~15% of peak shock wave pressure. Consequently, bubble pulse gives important dynamic loading to the underwater structure, and the effects of bubble pulse loading as well as shock wave loading should be considered to study the response of the underwater structure against underwater explosion of explosives. Bubble energy of EMX is 1.8MJ/kg and bubble energy of AL-EMX is 3.0MJ/kg.

Table 3 Similitude equations of sample explosives Sample explosive EMX AL-EMX Y K α K α Pmaxs MPa 39.0-1.1 37.5-1.0 θ/w 1/3 µs/kg 1/3 108 0.16 154 0.10 Is/W 1/3 Pa s/kg 1/3 5760 0.90 7290 0.93 EFDs/W 1/3 m kpa/kg 1/3 70.3-2.0 80.7-2.0 Pmaxb MPa 4.57-1.02 5.68-1.02 Ib/W 1/3 Pa s/kg 1/3 15000-1.1 18210-1.07 Y = K ( R/W 1/3 ) α FIGURE 8. EXAMPLE OF BUBBLE PULSE PROFILE FIGURE 9. EXAMPLE OF FIRST BUBBLE PULSE PLOFILE FIGURE 10. RELATION BETWEEN PEAK BUBBLE PULSE PRESSURE AND SCALED DISTANCE FIGURE 11. RELATION BETWEEN SCALED BUBBLE PULSE IMPULSE AND SCALED DISTANCE

CONCLUSIONS To measure underwater shock wave profile at the location very close to the explosive-water boundary, pressure gauge using fluoropolymer as sensing element was developed. Underwater shock wave profile was successfully measured in high pressure range where peak shock wave pressure exceeded 400MPa for EMX and AL-EMX. Bubble pulse profile was also precisely measured using pressure gauge using fluoropolymer. Following experimental results were obtained; (1) In the case of EMX, shock wave energy decreases with the increase of scaled distance in the scaled distance range smaller than 0.3 m/kg 1/3, due to the loss of shock wave energy by shock heating of surrounding water. However, in the case of AL-EMX, shock wave energy remains constant owing to shock wave enhancement due to the late energy release by aluminum reaction in detonation products. (2) Peak shock wave pressure of AL-EMX is almost same as that of EMX. Scaled shock wave impulse of AL-EMX is about 25% greater than that of EMX, and scaled shock wave energy flux density is about 15% greater than that of EMX within measured scaled distance range. (3) Peak bubble pulse pressure of AL-EMX is about 25% higher than that of EMX, and scaled bubble impulse is about 20% greater than that of EMX within measured scaled distance range. (4) The impulse of first bubble pulse is about 2.5 times greater than that of shock wave impulse, although peak pressure of first bubble pulse is only 10~15% of peak shock wave pressure. (5) The relations between peak shock wave pressure, scaled shock wave impulse, scaled shock wave energy flux density, peak bubble pulse pressure, scaled bubble pulse impulse and scaled distance are formulated in similitude equations. REFERENCES 1. Cole, R. H., Underwater explosions, Dover Publications, New York (1948). 2. Roth, J., Underwater explosions in Encyclopedia of Explosives and Related Items, Vol. 10, pp. U38-81, U. S. Army Research and Development Command, Dover, New Jersey (1983). 3. Murata, K., Takahashi, K., Kato, Y. and Murai, K., Development of pressure gauge using PVDF copolymer for underwater shock measurement, in APS Proceedings of Shock Compression of Condensed Matter-1995, American Institute of Physics, pp. 1093-1096 (1996). 4. Murata, K., Takahashi, K. and Kato, Y., Measurement of underwater shock wave by fluoropolymer sensor, Proceedings of 23 rd International Pyrotechnics Seminar, pp. 548-560 (1997). 5. Murata, K., Takahashi, K. and Kato, Y., Precise measurements of underwater explosion phenomena by pressure sensor using fluoropolymer, Journal of Materials Processing Technology, 85, pp. 39-42 (1999). 6. Sternberg, H. M. and Walker, W. A., Calculated flow and energy distribution following underwater detonation of a pentolite sphere, The Physics of Fluids, 14, pp. 1869-1878 (1971). 7. Hantel, L. W. and Davis, W. C., Spherical explosion in water, Proceedings of 5 th Symposium (International) on Detonation, ACR-184 Office of Naval Research, Arlington, Virginia, pp. 599-604 (1970). 8. Sanchidrian, J. A., Numerical modeling evaluation of underwater energies, Propellants, Explosives, Pyrotechnics, 23, pp. 301-308 (1998).