HAL Id: jpa-00226671
https://hal.archives-ouvertes.fr/jpa-00226671
Submitted on 1 Jan 1987
HAL is a multi-disciplinary open access archive for the deposit and dissemination of sci- entific research documents, whether they are pub- lished or not. The documents may come from teaching and research institutions in France or abroad, or from public or private research centers.
L’archive ouverte pluridisciplinaire HAL, est destinée au dépôt et à la diffusion de documents scientifiques de niveau recherche, publiés ou non, émanant des établissements d’enseignement et de recherche français ou étrangers, des laboratoires publics ou privés.
J. Lee
To cite this version:
J. Lee. THE PROBLEMS IN DETONATION PHYSICS. Journal de Physique Colloques, 1987, 48
(C4), pp.C4-417-C4-432. �10.1051/jphyscol:1987432�. �jpa-00226671�
JOURNAL DE PHYSIQUE
Colloque C4, suppl6ment au n-9, Tome 48, septembre 1987
THE PROBLEMS IN DETONATION PHYSICS
J. LEE
Department of Mech. Engineering, Mc GiZZ University, Montrba 2 , Canada
1. Introduction
This Workshop has brought together specialists from various disciplines. The objective is to explore how the techniques in these different fields can contribute towards the solution of the detonation problem. This is not an easy task for each of us has to learn the special languages of the different disciplines in order to communicate. I hope that the presentations of the past four days have achieved this to a certain degree. What remains now is to get into the detonation problem itself. As an introduction to the subequent discussions that follow, I thought it best to outline in a fundamental way the major outstanding problems in detonation physics.
Detonation is essentially a macroscopic phenomenon. It is a strong compression shock wave driven (or sustained) by the energy release in the chemical reactions which are initiated by the shock wave itself. Chemical reactions occur at the molecular level where unstable molecules (reactants) break
down toforln more stable species (products) and release potential energy in the process. The quantum chemical study of the molecular bond structure is obviously important at this microscopic level of the detonation process. On the other hand, the potential energy released by the reacting molecules must thermally equilibrate bringing the products to a very high local thermodynamic rate (i. e. pressure and temperature). It is the subsequent relaxation of this high local thermodynamic state that generates and sustains the shock wave that propagates into the reactants.
The shock wave in turn initiates further chemical reactions: either thermally via adiabatic compressional heating or mechanically via the generation of shear (and turbulence). Shock wave compression, shock wave interactions, and the generation of shear and turbulence are all macroscopic processes, belonging to the realm of hydrodynamics and thermodynamics. It is a formidable task to bridge the gap between
Article published online by EDP Sciences and available at http://dx.doi.org/10.1051/jphyscol:1987432
microscopic and macroscopic processes differing in length scales by at least five orders of magnitude. Molecular dynamical calculations which describe the detailed dynamics of typically about lo4 particles do not provide a true macroscopic description. In fact the thermodynamic quantities (such as pressure, temperature, particle velocity, etc.) and the macroscopic phenomena (i.e. sound and shock waves, heat transport, etc.) as deduced from molecular dynamical computations must be interpreted with great caution. The mechanical equations of motion (Hamiltonian, Lagrangian or Newtonian) used to describe the dynamics of the molecules are invariant to time reversal. Strictly speaking, the concept of thermal equilibrium, irreversibility and dissipative processes have no significance in molecular dynamics.
Numerical modelling of the hydrodynamic equations is on the macroscopic level, the results of which are directly comparable to experimental measurements. However, empirical input must be provided in the form of the equation of state, transport properties as well as chemical kinetic constants for the chemical reactions. If one is not careful there are sufficient degrees of freedom provided by these empirical constants for the numerical results to fit any experimental data even when the mechanisms are incorrect. Thus good agreement with experiments does not necessarily provide the correct test for the validity of the numerical model.
In the past four days, we have heard presentations on quantum chemistry spectroscopy, chemical kinetics, molecular dynamics, numerical modelling at the hydrodynamic level, as well as experiments on actual detonation processes. Let us now focus on how to tie these various fields together to solve the outstanding problems. In what follows, I hope to outline briefly the fundamental detonation problems and open the floor to discussion.
2. The Basic Ouestions
Almost all research in detonation physics is centered around the following questions: Given an explosive at given initial and boundary conditions, i) what are the steady detonation states (i.e. detonation velocity, pressure, temperature, products concentration, etc.)? ii) what are the dynamic detonation parameters (i.e. critical diameter, initiation energy, shock sensitivity, etc.)? and iii) is transition from deflagration to detonation
(DDT)possible and if so, what is the transition distance?
Initial condition refer to the type of explosive, its composition density,
grain size, physical dimensions, geometry and other physical,
thermodynamical and chemical properties. The type and the energy time characteristics of the ignition or initiation source can be included in the specification of the initial conditions. Boundary conditions mainly refer to the degree of confinement and properties of the confining surfaces.
Current experimental work is aimed at direct measurements of the detonation states, dynamic detonation parameters, and transition distances. The ultimate objective of detonation research is to achieve a-priori predictions of all these quantities, preferably from first principles.
3. Current Status
i) Steadv detonation states
According to classical theory, the Chapman-Jouguet criterion (i.e.
detonation velocity equals the sound speed in the product gases, D
=U1 +
C1) provides the missing link to close the set of conservation equations across the detonation front. For given explosive and initial conditions, the steady detonation states can be determined via an equilibrium thermodynamic calculation provided that the equation of state is specified.
The Chapman-Jouguet theory assumes equilibrium at the C-J surface where D
-
U1 + C1 and the steady detonation states computed on the basis of this
criterion are referred to as Chapman-Jouguet (C-J) detonations. Three
problem areas arise in the determination of the steady detonation states in
general. The first is associated with the equation of state for condensed
media. Current equations of state are empirically obtained from fitting
with experimental Hugoniot data. The accuracies are uncertain when they
are extended beyond the range of the data base itself. The second problem
arises from the equilibrium of the product gases. For so called non-ideal
explosives, different components of the explosive may have quite different
equilibrium times. Thus overall chemical equilibration may not be obtained
at the C-J surface and the steady detonation states may be based only on
partial chemical equilibration. A typical example would be the
condensation of carbon in the product gases. The non-equilibrium
condensation kinetic processes must be accounted for in the C-J
calculations. The third difficulty in computing the steady detonation
states is due to the influence of boundary conditions. Strictly speaking,
C-J states are independent of boundary conditions. However, boundary
conditions control the non-equilibrium hydrodynamic processes in the
products which may influence the energetics of the reactions and hence the
detonation state. Low velocity detonation is an example of the influence
of boundary conditions on the steady detonation speed.
ii) Dynamic Parameters
The Chapman-Jouguet theory does not take into account the structure of the detonation wave. It is independent of the propagation mechanism.
The dynamic detonation parameters, on the other hand, are functions of the detonation wave structure or the non-equilibrium rate processes. The fundamental mechanism of detonation is not known at present. The classical Zeldovich-D8ring-Von Neumann (ZDN) model which assumes a one-dimensional shock followed by a reaction zone provides a plausible mechanism of propagation, i.e. adiabatic shock heating leading to thermal decomposition and subsequent chemical reactions. For the case of gaseous explosives where the equation of state is well known and the details of the chemical kinetic processes can also be adequately described, the ZDN detonation structure can be determined theoretically. However, one-dimensional ZDN
detonation structures have not been observed experimentally because they
have been proven to be unstable. In practice the detonation structure is cellular, formed by a series of interacting incidents, reflected (or transverse) shock and Mach waves. For gaseous explosives the cellular structure has been well documented using different techniques and the averaged dimensions of the detonation cells (or transverse wave spacing) have been measured for many common gaseous explosives. The use of the one- dimensional ZDN structure has failed to provide quantitative theories for the prediction of the dynamic parameters. However, using the experimentally measured cell size (transverse wave spacing) as a length scale to characterize the reaction zone thickness (instead of the idealized ZDN reaction zone length), good correlations between the dynamic parameters and the cell size can be obtained. In other words, empirical relationships and analytical theories exist to give the dynamic parameters as a function of the cell size. Thus for gaseous explosives, the knowledge of the cell size enables the dynamic parameters to be computed to acceptable accuracies. The prediction of the cell size from first principles (using more fundamental parameters such as kinetic rate constants) is still an outstanding problem.
For condensed phase detonations, there is strong experimental evidence
of a similar cellular structure as gaseous detonations. However, no
systematic attempts have been made to measure the cell size and attempt
correlations with the dynamic parameters as yet. The cell size for
condensed phase detonations may be an order of magnitude (or more) smaller
than that of gaseous explosives at normal pressures. This may present
experimental difficulties in the measurement of the cell size. However the
critical diameter (which in general is an order of magnitude greater than
the cell size) could be used as the fundamental length scale in this case.
It would be of interest to pursue such correlations between cell size (or critical diameter) with the other dynamic parameters. Prediction of cell sizes from first principles may not be forthcoming for some time. Since the initiation mechanism in condensed explosives may not be unique and may depend on the particular explosive and its structure, it is doubtful that a universal theory (or model) for condensed phase detonation can be formulated. Measurement of a length scale that can characterize the reaction zone may replace the difficult task of searching for the correct initiation mechanism, at least from a practical point of view.
iii) Transition
Why a deflagration transits to a detonation is not known. Perhaps it is a consequence of some fundamental law that an explosive always tends to maximize its burning rate. Thus depending on the boundary conditions, a deflagration may accelerate to become i) a fast deflagration, ii) a low velocity detonation or iii) a normal Chapman-Jouguet detonation. A maximum burning rate principle is essentially
astatement
ofinstability in the same spirit as transition from laminar to turbulent flow or a transition from conduction to cellular convection in the Bernard cell problem.
Transition from deflagration to detonation is a macroscopic phenomenon involving the non-linear coupling between hydrodynamics, thermodynamics and chemical reactions which provide the energy to drive the non-linear processes. The transition problem can be divided into two phases: the acceleration phase and the onset of detonation. The mechanisms for flame acceleration in gaseous explosives are well known although their quantitative descriptions are not likely to be forthcoming for a while.
The mechanisms for the onset of detonation in gaseous explosives have also
been identified and again their quantitative description is extremely
difficult . For condensed explosives neither the mechanisms of flame
acceleration nor the mechanisms responsible for the onset of detonation
have been clearly identified. Difficulty in direct optical observations of
condensed phase combustion and the rapid time and spatial resolutions of
the diagnostics required for other indirect measurements severely hinder
progress. The DDT problem is not likely to be resolved even for gaseous
explosives in the near future. Yet the DDT problem is perhaps the most
important one in detonation reserch for it is directly related to the
question as to why and how explosives detonate. The occurence of DDT
ensures that the explosive (and its boundary conditions) can sustain a
detonation. Quite often, very strong shocks are used to initiate a
detonation even though the explosive and its boundary conditions are
outside the limits. The ability to undergo a transition implies the ability to self zelzera- the conditions necessary for the rapid detonation processes in the explosive. The detonability of the explosive is thus unambiguously demonstrated.
4. Concludinp: Remarks
I have attempted to synthesize the wide spectrum of research efforts in
detonation physics into a few fundamental issues. I have also given a
brief account as to what I see is the current state of knowledge in the
resolution of these fundamental detonation problems. This I hope will
serve as an adequate starting point for the subsequent discussions that
follow. It may be redundant to point out that the central problem is
detonation and the various disciplines are to be applied to the resolution
of the detonation problem. It is really a question of finding the right
shoes to fit the feet and not vice versa. The success of any cooperative
effort between specialists of different disciplines depends very much on
the commitment of all concerned towards the solution of the central
problem. We have learned what each discipline can do, now we have to
critically examine their applicability to the detonation problem.
Remarques de
N . M A N S O Nl o La c e l e r i t e D e s t determinee p a r l l @ n e r g i e li b e r e e l o r s de l a r e a c t i o n chimique, diminuee eventuellement de "pertes". C e l l e s - c i sont & imputer &
l a presence des p a r o i s ( p e r t e de chaleur, f r o t t e m e n t ...) ou a l e u r absence ( d e t e n t e l a t e r a l e ) .
E l l e s ne peuvent e t r e totalement absentes que dans l e cas de detonation spherique ( l a q u e l l e e s t en quelque s o r t e auto-confinee). Par consequent pour
" c o n t r o l e r " t e l l e ou a u t r e t h e o r i e ( t e l ou a u t r e modele) du mecanisme de l i b e r a t i o n de l ' e n e r g i e , en se r e f e r a n t a l a c e l e r i t e de l a detonation, c ' e s t l a c @ l e r i t e de l ' o n d e de d e t o n a t i o n sph6rique d i v e r g e n t e q u ' i l f a u t connai- t r e .
2' Au s u j e t de l a comparaison des d e f l a g r a t i o n s e t de detonation.
a ) L ' e n e r g i e l i b e r e e e s t l a mPme, mais l e "couplage" e n t r e l e choc e t l a combustion e s t totalement d i f f e r e n t e t il n ' e x i s t e que t r e s exception- nellement des regimes de propagation des d e f l a g r a t i o n s
&c & l @ r i t e SF cons t a n t e .
b ) La t r a n s i t i o n des d e f l a g r a t i o n s en detonation i m p l i q u e l a f o r m a t i o n d'une onde de choc suffisamment f o r t e e t donc l ' a c c e l e r a t i o n du f r o n t de combustion. C ' e s t une c o n d i t i o n necessaire, mais nullement, en p r i n c i p e , s u f f i s a n t e . La t r a n s i t i o n se p r o d u i t l o r s q u e e n t r e l e f r o n t de choc e t c e l u i de combustion sont r e a l i s e e s l e s c o n d i t i o n s de p, de T e t de turbulence encore insuffisamment connues. Dans l e cas des ex-.
p l o s i f s condenses, e t a n t donne l e s c 6 l e r i t e s de propagation du f r o n t de combustion (mm/sec a quelques m/sec & haute pression), l a f o r m a t i o n d'une onde de choc f o r t e p a r a i t problematique,
&moins q u ' i l
ya i t un mecani sme.
R e m a r q u e d e C.
F A U Q U I G N O NLa t h e o r i e thermo-hydrodynamique de l a d e t o n a t i o n ne p a r a i t pas d e v o i r & t r e remise en cause s i l a charge explosive a des dimensions s u f f i s a n t e s pour qu'un regime monodimensionnel s t a t i o n n a i r e puisse & t r e e t a b l i e t que l e s diverses r e a c t i o n s chimiques a i e n t des c i n e t i q u e s v o i s i n e s .
Par contre, 1 'analyse microscopique (au sens p r e c i s e dans 1 ' a t e l i e r ) e s t ne- c e s s a i r e pour comprendre l e s processus de d i s s o c i a t i o n de l a molecule explo- s i v e d e r r i e r e l e f r o n t :
- La mise en evidence du champ e l e c t r i q u e dans l e f r o n t ( v o i r expose de M. PRESLES) e s t i n t e r e s s a n t e e t c o n s t i t u e 1 a premiere demonstration d'une r e g i o n hors e q u i l i b r e .
- Des analyses de ce tyDe a i n s i que des observations e t mesures de spec- t r o s c o p i e a c t i v e d e v r a i e n t c o n s t i t u e r l e s o u t i l s de l a recherche f u t u r e
& c o n d i t i o n d ' 6 t r e appl iquees & des e x p l o s i f s homogenes ( 1 iq u i d e s ) ou
& o r i e n t a t i o n ster6ochimique connue (monocristaux) .
R e m a r k s f r o m R. CHERET
When d e a l i n g w i t h e x ~ l o s i v e s , a PRACTICAL ISSUE i s a q u a n t i t a t i v e e s t i m a t i o n o f HAZARDS and EFFECTS o f a f i n i t e e x p l o s i v e s t r u c t u r e under a given e x c i t a - t i o n . The u l t i m a t e goal o f t h i s e s t i m a t i o n may be one o r several among t h e f o l l o w i n g :
- m i n i m i s i n g . a dimension,
. a t o t a l mass,
. a t o t a l volume,
. some c o s t / e f f e c t i v e n e s s r a t i o ,
. some f a i l u r e frequency,
. some t r i a l and e r r o r process expenses,
. e t c ...
- compromising w i t h a non-explosive p r o p e r t y such as thermomechanical behaviour, etc.. .
Thinking o f these p r a c t i c a l issues . ( t h e economical weight o f which must be k e p t i n mind) makes me uncomfortable d u r i n g these days because such a work- .shop does show which TOOL each o f us has and what he doing w i t h h i s t o o l ,
b u t does n o t show which t o o l ( s ) i s ( a r e ) a p p r o p r i a t e f o r a given PRACTICAL ISSUE.
L e t us consider an example : t h e problem o f t h e steady detonation v e l o c i t y D i n a l o n g plastic-bonded s o l i d e x p l o s i v e rod, surrounded by a g i v e n medium m.
This v e l o c i t y D depends on t h e diameter B o f t h e rod, on t h e i n i t i a l temper- ature, on some parameters o f t h e aggregate (mean g r a i n diameter
6f o r example) and some parameters o f t h e surrounding medium. Yodeling D r e q u i r e s many t o o l s .
- continuum mechanics a t 0 l e v e l ,
- continuum thermodynamics a t
6l e v e l ,
- quantum s t a t i s t i c a l mechanics a t molecular l e v e l .
A l l these t o o l s have been separately discussed d u r i n g t h i s workshop; b u t t h e use o f modern methods o f MULTIPLE SCALING which enable t o combine the t o o l s has n o t even been mentioned.
I n o t h e r terms and i n conclusion, I would l i k e t o p o i n t o u t t h a t much
r e c e n t progress i n t h e f i e l d o f combustion and explosions has o r i g i n a t e d from
t h e use o f t h e FlULTIPLE SCALING methods, and t h a t much more i s s t i l l t o come.
VOIES DE RECHERCHES
1 .
I n t e r v e n t i o n d e J.
B O I L E A ULes suggestions pour des voies de recherches p o r t e r o n t s u r t r o i s p o i n t s : l e s e x p l o s i f s primaires, c e r t a i n s melanges, l e s oolymeres e x p l o s i f s .
1 - E x p l o s i f s primaires. DiamPtres c r i t i q u e s .
L ' o b j e c t i f e s t de chercher d comprendre ce qui. se passe e n t r e l e nanometre e t l e m i l l i m e t r e , e t donc d l & t u d i e r l e s e x o l o s i f s p r i m a i r e s e t l a faqon dont s ' y developpe e t s ' y propage 1 a detonation.
- Y a - t - i l pour l e s e x p l o s i f s p r i m a i r e s un oassaqe d i r e c t de l ' i n i t i a - t i o n ?I l a detonation ou y a - t - i l t r a n s i t i o n p a r d e f l a g r a t i o n i n t e r m e d i a i r e ? S i o u i , comment l ' o b s e r v e r , comment mesurer l a longueur de l a zone de reac- t i o n ? e s t - e l l e f o n c t i o n de l a nature e t de l l i n t e n s i t @ de l ' i n i t i a t i o n ?
- Si l a mesure d i r e c t e e s t t r o p d i f f i c i l e , que se p a s s e - t - i l s i l ' o n melange 1 'e x p l o s i f p r i m a i r e avec a u t r e chose ( e x p l o s i f secondaire, d i l uant i n e r t e s o l i d e , d i l u a n t i n e r t e l i q u i d e , s o l v a n t ) ?
- Y - a - t - i l deux s o r t e s d ' e x p l o s i f s p r i m a i r e s , ceux q u i sont " s t a b l e s "
e t pour l e s q u e l s une i n i t i a t i o n d ' i n t e n s i t e non n e g l i g e a b l e e s t necessaire (par ex. azide de plomb) e t ceux q u i sont t e l l e m e n t i n s t a b l e s que c e t t e
~ n i t i a t i o n peut & r e extremement f a i b l e pour provoquer l e u r d e t o n a t i o n ( p a r ex. N H, ou HNF2 s o l i d e ...). O n t - i l s des courbes de p o t e n t i e l s d ' e t a t fondamenta? d i f f e r e n t e s , ou b i e n ne s ' a g i t - i l que d ' une v a l e u r d i f f e r e n t e des s e u i l s d ' e x c i t a t i o n ?
2 - Melanges.
On peut certainement o b t e n i r des renseignements i n t e r e s s a n t s p a r t i r de me1 anges.
- Melanges homogPnes, p a r exemple de l i q u i d e s , d'eutectiques, de c r i s - t a u x s y n c r i s t a l l i s ~ s ; comparaison de deux e x p l o s i f s l i q u i d e s , l ' u n forme de molecules d'un seul p r o d u i t , l ' a u t r e de deux l i q u i d e s m i s c i b l e s , l ' u n oxydant, l ' a u t r e combustible, l e melange ayant une composition g l o b a l e v o i - s i n e de c e l l e du premier ~ r o d u i t . Etude du nitromethane s e n s i b i l i s e par une ami ne.
- Melanges h@t&rogenes avec une phase continue e t une phase g r a n u l a i r e , en f o n c t i o n du taux de l a phase g r a n u l a i r e au voisinage du taux de percola- t i o n ; en f o n c t i o n de l a t a i l l e des grains, descendant j u s q u ' i i quelques nano- metres.
3 - Polymeres e x p l o s i f s .
U t i l i s a t i o n de polymeres e x p l o s i f s homogenes e t b i e n c a r a c t e r i s @ s , comme materiau d'etude : avantages, d i f f i c u l t e s ? On Dourra prendre comme e x p l o s i f de base l e n i t r a t e de p o l y v i n y l e . On oourra f a i r e v a r i e r sa s t r u c t u r e ( n a t u r e des enchainements), sa composition ii p a r t i r des copolymeres avec des carbonates de v i n y l e n e ou de m@thylvinyl@ne. On peut f a i r e v a r i e r sa s t r u c - t u r e de facon continue, f a i r e une etude f i n e autour,des p o i n t s de t r a n s i - t i o n ; on peut mPme c r e e r des s t r u c t u r e s p l u s ou moins ordonnees, par modi- f i c a t i o n des polymeres t e l l e s que des i n s e r t i o n s de grouoes mesogenes ( s t r u c t u r e s nematiques ou smectiques).
I 1 f a u t n o t e r e t s o u l i g n e r e n f i n une p r o p o s i t i o n de recherche f a i t e par
M. de L o n g u e v i l l e : m o d i f i c a t i o n d'une onde de detonation en regime s t a t i o n -
n a i r e par une p e r t u r b a t i o n .
2.
I n t e r v e n t i o n d e A.
RENLUD"Simple" shock-induced chemistry i n non-expl osives.
- Are shocks thermal ?
- How does mechanical shock promote r e a c t i o n ? I d e a l e x p l o s i v e systems.. . 1 iq u i d , s i n g l e c r y s t a l
- more exoerimental methods a r e u s e f u l
- Results may be modeled Granular "pure" explosives
- m a t e r i a l v a r i a b l e s
- i n i t i a t i o n surface
- s u b - i n i t i a t i o n t h r e s h o l d
- steady-state detonation.
3.
F u t u r e of C h e m i c a Z K i n e t i c s in D a t o n a t i o n
: C. M E L I U SA - Coupling o f Chemical Reactions w i t h F l u i d Mechanics.
B - D i s t i n g u i s h i n g the d i f f e r e n t Reaction Stages.
I ) Decomposition 2 ) Heat Release
3 ) Intermediate StagesC - Coupling Experiment and Theory.
1) Species I d e n t i - f i c a t i o n
2 ) Regimes : Thermal Decomposition, D e f l a g r a t i o n , Detonation.
4.
M o d e Z Z i n g I n i t i a t i o n / Detonation. " C r i t i c a Z I s s u e s "
:J. N U N Z I A T O Hot Spots
.. Mechanism o f Formation
Pore c o l l a p s e vs. shear band Mechanism f o r Hot Spot decomposition
Thermally a c t i v a t e d vs. bond s i s s i o n Role o f Hot Spots i n Detonation
D e t a i l e d Chemical K i n e t i c s
- 0
Best estimates o f r e a c t i o n oaths
Rate oarameters
- *
Role o f phase changes (me1 t i n g ) Endothermic r e a c t i o n s
Pressure ( d e n s i t y ) e f f e c t s n n condensed phase r e a c t i o n s
- Numerical M o d e l l i n g (continuum) o f I n i t i a t i o n / Oetonatiorl
Provides answers, i d e n t i f i e s s e n s i t i v e parameters, guides exoeriments, t i e s experiments t o g e t h e r
.. F l u i d / S o l i d mechanics. "Hot Spots"
Chemical K i n e t i c s
- ZND/CJ Theory
D e t a i l e d k i n e t i c s Products EOS
- I n s t a b i l i t i e s
- Boundary Conditions Computational Methods (Hardware)
Remarks o f D . T S A I a f t e r t h e Megeve W o r k s h o p