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Journal ArticleDOI

Combustion Characteristics of Iso-Octane/Hydrogen Flames under T and P Effects up to near Flammability Limits

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In this paper , the authors investigated the combustion characteristics of iso-octane flame with 0% and 30% H<sub>2</sub> up to near lean limits (λ = 1.8-1.7) at 100-300 kPa and 393-453 K.
Abstract
<div class="section abstract"><div class="htmlview paragraph">Lean combustion is an approach to achieving higher thermal efficiency for spark ignition engines. However, it faces low burning velocity and unstable combustion problems near the lean flammability limits region. The current work is attempting to investigate the combustion characteristics of iso-octane flame with 0% and 30% H<sub>2</sub> up to near lean limits (λ = 1.7) at 100-300 kPa and 393-453 K. The flame appeared spherically by 37 mJ spark energy at λ = 0.8-1.2, whereas the ultra-lean mixtures, λ ≥ 1.3, ignited at 3000 mJ under wrinkles and buoyancy effects. The impact of initial pressure and temperature on the lean mixture was stronger than the stoichiometric mixture regarding flame radius and diffusional-thermal instability. The buoyancy appeared at the highest burning velocity of 27.41 cm/s. The buoyancy region extended from λ = 1.5 to λ = 1.3 at 393 K, λ = 1.6 to λ= 1.4 at 423 K and λ = 1.7 to λ = 1.5 at 453 K with an increase in initial pressure (higher pressure, more λ under buoyancy effect), but initial temperature decreased the region from λ= 1.5 to λ = 1.7 at 100 kPa, λ = 1.4 to λ = 1.6 at 200 kPa and λ = 1.3 to λ = 1.5 at 300 kPa. OH mole fraction <7.6642×10<sup>-3</sup> for H<sub>2</sub> = 0% and <7.7765×10<sup>-3</sup> for H<sub>2</sub> = 30% required 3000 mJ for ignition at 393 K and 100 kPa, and buoyancy appeared at ≤4.8788×10<sup>-3</sup> for H<sub>2</sub> = 0% and ≤4.9547×10<sup>-3</sup> for H<sub>2</sub> = 30%.</div></div>

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References
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Journal ArticleDOI

A comprehensive modeling study of hydrogen oxidation

TL;DR: A detailed kinetic mechanism has been developed to simulate the combustion of H2/O2 mixtures, over a wide range of temperatures, pressures, and equivalence ratios as discussed by the authors.
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TL;DR: In this article, an improved version of the kinetic model was used to analyze the combustion behavior of several components relevant to gasoline surrogate formulation, focusing attention on the mixing effects of the fuel components.
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The measurement of laminar burning velocities and Markstein numbers for iso-octane-air and iso-octane-n-heptane-air mixtures at elevated temperatures and pressures in an explosion bomb

TL;DR: In this article, the effects of the initial mixture temperature and pressure on these parameters also have been examined and data have been obtained for iso-octane-air mixtures at initial temperatures between 358 K and 450 K, at pressures between 1 and 10 bar, and equivalence ratios, φ, of 0.8 and 1.0.
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