Luiz Maltez Faria’s research while affiliated with University of Paris-Saclay and other places

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Publications (3)


Fig. 3 a D-c f curves and b integrated chemical times, τ chem , obtained with the detailed mechanism of Ó Conaire et al. [35]. The horizontal dotted line denotes the limit between the quasi-detonation and choking regimes. The round markers in (a) indicate the points at which the p, T , u, ˙ σ , and Y k profiles are analyzed. The D/D CJ value at which the first turning point occurs for each mechanism is also included in (a). The intensity change of the lines in (b) represents the scaled friction coefficient, c f /c f,crit , for a given value of D/D CJ
Fig. 6 D(c f,crit ) variation with activation energy for different similarity factors α. The thick black lines depict the results obtained with the analytical expressions using high activation energy asymptotics developed by Zel'dovich et al. [37] and taken from Higgins' chapter [22] for detonations with heat losses only (top) and a combination of heat and friction losses with = 1.5 (bottom). The shadowed region indicates the upper/lower limit of the theoretical expression with the parameter ∈ [0.9, 1.8]
Heat and momentum losses in H2{\text {H}}_{2}O2{\text {O}}_{2}N2/Ar{\text {N}}_{2}/{\textrm{Ar}} detonations: on the existence of set-valued solutions with detailed thermochemistry
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June 2024

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77 Reads

Shock Waves

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L. Faria

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The effect of heat and momentum losses on the steady solutions admitted by the reactive Euler equations with sink/source terms is examined for stoichiometric hydrogen–oxygen mixtures. Varying degrees of nitrogen and argon dilution are considered in order to access a wide range of effective activation energies, Ea,eff/RuT0E_{\textrm{a,eff}}/R_{\textrm{u}}T_{0} E a,eff / R u T 0 , when using detailed thermochemistry. The main results of the study are discussed via detonation velocity-friction coefficient ( D – cfc_{\textrm{f}} c f ) curves. The influence of the mixture composition is assessed, and classical scaling for the prediction of the velocity deficits, D(cf,crit)/DCJD(c_{\textrm{f,crit}})/D_{\textrm{CJ}} D ( c f,crit ) / D CJ , as a function of the effective activation energy, Ea,eff/RuT0{E}_{\textrm{a,eff}}/R_{\textrm{u}} T_{0} E a,eff / R u T 0 , is revisited. Notably, a map outlining the regions where set-valued solutions exist in the Ea,eff/RuT0αE_{\textrm{a,eff}}/R_{\textrm{u}}T_{0}\text {--}{\alpha } E a,eff / R u T 0 -- α space is provided, with α\alpha α denoting the momentum–heat loss similarity factor, a free parameter in the current study.

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Influence of chemistry on the steady solutions of hydrogen gaseous detonations with friction losses

February 2022

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224 Reads

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12 Citations

Combustion and Flame

The problem of the steady propagation of detonation waves with friction losses is revisited including detailed kinetics. The derived formulation is used to study the influence of chemical modeling on the steady solutions and reaction zone structures obtained for stoichiometric hydrogen-oxygen. Detonation velocity-friction coefficient (D − c f) curves, pressure, temperature , Mach number, thermicity and species profiles are used for that purpose. Results show that both simplified kinetic schemes considered (i.e., one-step and three-step chain-branching), fitted using standard methodologies, failed to quantitatively capture the critical c f values obtained with detailed kinetics; moreover one-step Arrhenius chemistry also exhibits qualitative differences for D/D CJ ≤ 0.55 due to an overestimation of the chemical time in this regime. An alternative fitting methodology for simplified kinetics is proposed using detailed chemistry D − c f curves as a target rather than constant volume delay times and ideal Zel'dovich-von Neumann-Döring profiles; this method is in principle more representative to study non-ideal detonation propagation. The sensitivity of the predicted critical c f value, c f,crit , to the detailed mechanisms routinely used to model hydrogen oxidation was also assessed; significant differences were found, mainly driven by the consumption/creation rate of the HO 2 radical pool at low postshock temperature.


Figure 1: Schematic of experimental setup showing front and side view of the 6 mm × 6 mm channel (not to scale).
Figure 3: DDT stages for stoichiometric H 2 -O 2 in a 6 × 6 mm channel. Initial conditions: p 0 = 100 kPa, T 0 = 295 K. Time interval between frames: ∆t = 5 µs for laminar flame propagation, development of flame instabilities and formation of waves ahead of flame; ∆t = 2.5 µs for DDT and detonation propagation.
Figure 6: Structure of co-existing traveling wave solutions admitted by Eq. (1) -scalar variable, u (dashed-dotted line), unsteady term, u t (dashed line), and budgets (solid lines): convection -black; friction losses -red; heat release -blue.
Figure 7: Qualitative comparison of the transition dynamics -Left: scalar model with generic losses. Right: experimental observations (right).
Experimental and theoretical observations on DDT in smooth narrow channels

August 2020

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184 Reads

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13 Citations

Proceedings of the Combustion Institute

A combined experimental and theoretical study of deflagration-to-detonation transition (DDT) in smooth narrow channels is presented. Some of the distinguishing features characterizing the late stages of DDT are shown to be qualitatively captured by a simple one-dimensional scalar equation. Inspection of the structure and stability of the traveling wave solutions found in the model, and comparison with experimental observations, suggest a possible mechanism responsible for front acceleration and transition to detonation.

Citations (2)


... For hydrocarbon-air detonations, a two-step approach requires transporting seven species [28]. Three-step mechanisms further split the chemical process into chain-initiation, chain-branching, and termination steps [2,29]. However, the three-step mechanisms produce weaker transverse waves, larger instantaneous flow structures, and different quenching limits compared to detailed mechanisms. ...

Reference:

Tabulated chemistry approach for detonation simulations
Influence of chemistry on the steady solutions of hydrogen gaseous detonations with friction losses

Combustion and Flame

... These observations provide further evidence of the role played by walls on flame acceleration, most probably through the formation of favorable thermal gradients 54,55 due to friction induced heating within the hydrodynamic boundary layer. [56][57][58] During the combustion process, due to the uneven rates of molecular diffusion and thermal diffusion, there is a thermal diffusion instability at the flame front, leading to pronounced wrinkles at the flame front. These wrinkles increase the contact area between the flame and the surrounding gas, promoting gas mixing and diffusion, and thus accelerating the flame propagation, as illustrated by the iso-lines of heat release in Fig. 8. ...

Experimental and theoretical observations on DDT in smooth narrow channels

Proceedings of the Combustion Institute