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A facility for simulating the dynamic response of materials

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equation of state of unreacted nitramine explosives, polymers ... Use of POOMA solvers written as Python extensions as a PSE for EL computations. Julian Cummings. ... – PowerPoint PPT presentation

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Title: A facility for simulating the dynamic response of materials


1
A facility for simulating the dynamic response of
materials
  • High Explosives
  • Joe Shepherd
  • Caltech
  • ASCI ASAP Site visit
  • Oct. 10-11,2000

2
Description and goals of subproject
  • Molecular properties and reaction rates
  • chemistry of nitramine reactions
  • molecular dynamics of shock initiation
  • equation of state of unreacted nitramine
    explosives, polymers
  • High explosive simulation capabilites
  • AMR and GFM methods for VTF
  • reaction mechanism reduction for detonation
    simulations
  • Engineering models of High Explosives
  • implement and test EoS and reaction models
  • cylinder test
  • corner turning

3
Personnel
  • Faculty
  • JE Shepherd
  • WG Knauss
  • P. Tang
  • Staff
  • S. Dasgupta (MP)
  • R. Muller (MP)
  • E. Morano
  • J. Cummings (CACR)
  • R. Samtaney (CT)
  • Postdocs
  • G. Caldwell (MP)
  • D. Chakraborty (MP)
  • A. Strachan (MP)
  • S. Sundaram
  • Students
  • M. Arienti
  • C. Eckett
  • P. Hung

FY00 Alumni FY00 additions
4
How subproject integrates into the VTF
5
Interactions with other subprojects
  • Develop engineering models of HE and provide to
    VTF team
  • Equation of state
  • Reaction rate
  • Work with SD to couple to FEM solid simulations
  • Develop and verify Eulerian-Lagrangian coupling
    schemes and provide to VTF team
  • Use MP reaction rate model for nitramines as
    input to ILDM models
  • Use MP Molecular Dynamics simulation for HE EoS
  • Work jointly with MP on shock initiation of HE

6
Response to FY99 review
  • Caution is offered with respect to the use of the
    ILDM procedure for detonation reaction mechanism
    reduction . strategic planning with respect
    to alternatives for reaction mechanism reduction
    is recommended.
  • Augmented ILDM method (induction manifold ILDM)
    was successful! Method was implemented,
    verified, and validated against 2D detailed
    chemistry simulation.
  • Risk-taking was justified in this case -
    potential risk was more than offset by enormous
    benefits of success.

7
Research activities in FY00
  • Detailed reaction mechanisms for nitramines
  • Condensed phase effects on reactions
  • Molecular dynamics of shock initiation
  • Reactive force field treatment of nitramines
  • Reduced reaction mechanism via ILDM
  • Engineering models of HE
  • improved product EoS, initial temperature effects
  • Parallel AMR-GFM method for HE simulation with
    realistic boundary response
  • Evaluation of GFM implementation schemes
  • transparency acceleration tests

8
Computational Science interactions
  • Use of GrACE C library for AMR
  • Manish Parashar
  • Use of Python to script FEM and EL test problems
  • Michael Aivazis
  • Use of POOMA solvers written as Python extensions
    as a PSE for EL computations
  • Julian Cummings.

9
Achievements in basic science/engineering
  • Nitramine chemistry
  • detailed gas phase reaction mechanism for HMX
    RDX
  • reactive force field developed for nitramines
  • molecular dynamic simulation of shock-initiated
    RDX
  • EoS of shocked HE and polymers
  • Reaction Mechanism Reduction
  • 4D ILDM computed for H2-O2-Ar
  • ILDM induction manifold implemented in 2D AMR
    gas detonation
  • GFM validations
  • AMR GFM implemented in 2D
  • 2D AMR detonation in elastic tube simulation
    carried out
  • Implemented JTF EoS model for PBX in 3D AMR
    solvers

10
Accomplishment of MP group in HE
  • Reaction mechanism for nitramines
  • HONO elimination
  • RDX HMX mechanism completed
  • Reactive force field for nitramines
  • shock simulations of initiation in DMNA,
    RDX
  • Polymer EoS
  • computation of Gruneisen coefficients, shock
    Hugoniots

11
RDX mechanism
  • Starting point
  • GRI nitromethane mechanism (49 species, 300
    reactions)
  • Melius nitromethane mechanism (27 species, 130
    reactions)
  • Yetter RDX mechanism (48 species, 240 reactions)
  • Extension
  • DFT-B3LYP/6-31G theory structure for all
    reactants, intermediates (13), transition states
    (14) and products
  • Analytical frequencies for all species
  • Incorporation of detailed kinetics for early
    stage CHNO reactions
  • Overall scheme
  • 85 species, 461 reactions
  • Thermochemical data for all new species
  • Theoretical rate constants - RRKM/TST
    calculations
  • J. Phy. Chem. A, 104, 2261-2272, 2000.

12
Unimolecular Decomposition of RDX
13
HMX mechanism summary
  • NO2 elimination via NN bond dissociation leading
    to HMR (radical) subsequent decomposition to
    smaller products
  • Successive 4 HONO elimination and further
    decomposition of both HONO and the mass 108
    intermediate
  • O migration from NO2 to adjacent C forming open
    ring RDX structure and oxy-ring MN structure
    which undergo further decomposition
  • NN homolysis pathway (1) connects HMX
    decomposition to RDX decomposition network

14
Shock simulation of RDX using Reactive FF
Impact velocity
2km/sec
3km/sec
32 RDX molecules 672 atoms
Reaction above threshold up
15
Reaction Products
  • 2km/s - no reaction
  • some conformational changes w.r.t. NO2
    orientation
  • 3km/s - extensive reactions
  • Major species formed
  • HONO
  • NO2, H2O
  • O2, N2, NO, OH
  • H2CNO2, H2CN, H2CN-NO

16
ILDM Reaction Mechanism Reduction
  • 22 dimensional ILDM for H2-air

17
Cellular Detonation Simulations
  • Self-propagating (not overdriven) cellular
    detonation in H2O27Ar (Oran et al. 1998)
  • Finest grid level 256 mesh cells across channel,
    10 mesh cells per ZND induction length, AMR
    (Amrita)

18
Transparency Test
19
2D Validation test of GFM
  • superseismic shock wave--elastic solid wave
    interaction

20
2D AMR GFM
  • 2D AMR HMX detonation simulation
  • FEM Copper simulation
  • GFM

21
Corner turning in HMX
AMR (60x40) mesh refined twice with ratio 2, 10
processors
22
Application of Model - T-effect in TATB
  • Both the detonation velocity and the CJ pressure
    increase as the temperature goes down
  • There is no performance degradation from cold in
    plane geometry
  • Performance degradation comes from the slowing
    down of the propagation velocity in corner
    turning and divergence
  • Performance degradation comes from larger
    unburned region
  • Reaction model with kinetics is needed to address
    this issue

23
Integrated 3D Parallel Simulation
  • Adlib solid tantulum model, Cohen thermal EoS, J2
    plasticity
  • RM3D fluid model with Morano MG HMX model 66 Gpa
    CJ pressure
  • ASCI Blue Pacific 1024 processors

24
Tasks for FY00
  • Materials properties
  • Complete reaction network for nitramines
    COMPLETED
  • Investigate via MD early events in shocked high
    explosives IN PROGRESS
  • Engineering model
  • Reduced reaction network for nitramines and
    application to 1-D and 2-D detonation Developed
    ILDM method in FY00
  • Integration of JTF models utilizing reduced
    reaction networks into 3-D Eulerian code Delayed
    to FY01
  • Integrated simulation
  • Develop 3-D Eulerian AMR simulations of
    detonation with GFM IN PROGRESS

25
Status of Milestones for FY00
  • 2-D parallel engineering model detonation
    calculations utilizing integrated VTF Q1 FY00 ?
  • 3-D parallel engineering model detonation
    simulations using AMR Q3 FY00 ?- in place, 2D
    runs only so far
  • Fully 3-D coupled Eulerian/Lagrangian simulation
    using ghost fluid method Q4 FY00 ?
  • Simulation utilizing materials database Q1 FY01
  • under development

26
Validation
  • AMR
  • backward-facing step
  • cylindrical shock
  • GFM
  • 1D piston tests
  • 1D shock transparency tests ( EL, LE)
  • 2D convergence and mass conservation tests
  • 2D cylinder lift-off test
  • 2D super-seismic shock wave propagation along
    elastic boundary
  • ILDM
  • ZND, CV,Oran et al 2D simulations

We need access to high-quality data on
  • Corner-turning experiments
  • Cylinder test experiments
  • Initiation experiments

27
Leveraging
  • Navy MURI on Pulse Detonation Engines
  • Using POOMA-based FEM methods to model transient
    response of structures loaded by shock and
    detonation waves. Experimental research on
    elastic waves and fracture used in code
    validation.

28
Plans for FY01
  • Reaction Rates and Early Events in Shocked HE
  • joint work with MP group, effects of high density
  • ILDM method for HE
  • apply methods developed in FY00 to nitramines
  • Engineering Models for HE
  • next generation reaction model
  • Integrated Simulations for HE
  • transfer AMR-GFM methodology to VTF
  • initiation, corner turning, cylinder test
  • validation against experiments

29
Milestone for FY01
  • Performance of a large-scale parallel simulation
    of detonation propagation with an advanced model
    of the reaction zone. Q3 FY 01.
  • Tasks
  • 1. Develop revised, robust mixture equation of
    state
  • 2. Implement AMR solution of multi-species
    reaction model
  • 3. Develop ILDM reduced model of chemical
    reaction network
  • 4. Verification and Validation testing
  • 5. Large-scale demonstration simulation.

30
Interactions with other ASAP centers
  • Developing collaboration with Illinois center
    (Scott Stewart) on detonation models and EL
    coupling methods.

31
Interactions with DP laboratories
  • Transferred nitramine reaction mechanism to LLNL
  • Nick Winter, Bill Pitz, Larry Fried
  • POOMA (LANL)
  • Julian Cummings (now at CIT)
  • Engineering models of HE (LANL)
  • Pier Tang (now at CIT)

32
Publications
  • Eckett, Quirk, Shepherd The role of unsteadiness
    in the direct intiation of gaseous detonation
    JFM 421, 147-183, 2000.
  • Reduced reaction models for detonation
    simulation, in preparation.
  • A simplified model of high explosive
    detonation, in preparation.
  • Eulerian-Lagrangian Coupling Schemes, in
    preparation.
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