Jacqueline Beckvermit
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1 Jacqueline Beckvermit Monica Hall Dr. Todd Harman Dr. Martin Berzins Dr. Charles Wight XSEDE 13
2 Analyze the effects of the heat flux and heating geometry on the cook-off response of an explosive device Understand the underlying mechanism(s) of a Deflagration to Detonation Transition
3 Background on Energetic Materials Uintah Computational Framework Cook-Off Results Future Research
4 Octahydro-1,3,5,7-tetranitro- 1,3,5,7- tetrazocine (HMX) PBX9501 (Plastic Bonded Explosive)
5 Deflagration Convective and Conductive Deflagration
6 Deflagration Convective Deflagration Convective and Conductive Deflagration Conductive Deflagration Asay, B.w., S.f. Son, and J.b. Bdzil. "The Role of Gas Permeation in Convective Burning."International Journal of Multiphase Flow 22.5 (1996): Print.
7 Asay, B.w., S.f. Son, and J.b. Bdzil. "The Role of Gas Permeation in Convective Burning."International Journal of Multiphase Flow 22.5 (1996): Print.
8 Deflagration Convective and Conductive Deflagration Detonation
9 Deflagration Convective and Conductive Deflagration Detonation Deflagration to Detonation Transition (DDT) Shock to Detonation Transition (SDT)
10 Material Point Method (MPM) Lagrangian Condensed phase models Multi-material CFD formulation (ICE) Finite volume-eulerian Gas phase models MPM-ICE Lagrangian/Eulerian Solves fluid-structure interactions J. Guilkey, T. Harman, and B. Banerjee. An Eulerian-Lagrangian approach for simulating explosions of energetic devices. Computers and Structures, 85: , 2007.
11 Global Kinetics Model represents the physics and chemistry of macroscopic energetic material combustion Breaks energetic material combustion into two parts Condensed phase Gas phase
12 Ward Son Brewster (WSB) Model Burn model ViscoScram Isotropic damage model Stress depended cracking JWL ++ Detonation model Validation J. Peterson and C. Wight. An Eulerian-Lagrangian computational model for deflagration and detonation of high explosives. Combustion and Flame, page in press, 2012.
13 MPM-ICE Scalable up to 256K Cores AMR MPMICE: Scaling Mean Time Per Timestep (s) 10 1 Strong Weak K 2K 4K 8K 16K 32K 64K 128K256K Cores
14 Heat flux and heating geometry effects on a cook-off response Deflagration to Detonation Transition mechanism
15 PBX 9501
16
17 Detonation Case Burst
18
19
20
21 Under adiabatic conditions deflagration of PBX9501 will reach ~2 GPa Detonation requires 5.3 GPa Where did the other 3.3 GPa come from?
22 20 μsec 120 μsec PBX Temp Pressure Gas Temp Reacting PBX 130 μsec 140 μsec
23 170 μsec 171 μsec 172 μsec 5.30 GPa 3.97 GPa 2.65 GPa 1.32 GPa 1e-4 GPa
24
25 25 μsec PBX Temp 170 μsec Pressure Gas Temp Reacting PBX 175μsec 185 μsec 185 μsec
26 192 μsec 193 μsec 194 μsec 195 μsec 5.30 GPa 3.97 GPa 2.65 GPa 1.32 GPa 1e-4 GPa
27
28 Detonation occurs from two colliding pressure waves Lower heat flux is more likely to detonate One sided heating is more likely to detonate
29 Pressure amplification as a function of mass burned Look at large scale simulations to determine a critical density for transporting explosives
30 "Truck Explosion Leaves Huge Crater On Highway." DREAMS OF THE GREAT EARTH CHANGES. Web. 25 Feb <
31 80,000 Processors on Titan 1m x 1m x 1m Domain 6,000 Processors on Stampede 1.2m x 0.8m x 0.2m Domain
32 Monica Hall Dr. Charles Wight Dr. Todd Harman Dr. Martin Berzins Andrew Bezdjian
33 160 1 Side 2 Sides 140 Threshold Heat Flux (kw/m 2 ) x80 85x85 90x90 95x95 100x100 Device Dimensions (mmxmmx1mm)
34
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