Jihad Badra - Academia.edu (original) (raw)

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Papers by Jihad Badra

Research paper thumbnail of Characteristics of spray from a GDI fuel injector for naphtha and surrogate fuels

Research paper thumbnail of Chemical Kinetic Insights into the Octane Number and Octane Sensitivity of Gasoline Surrogate Mixtures

Research paper thumbnail of A shock tube study of C4–C6 straight chain alkenes + OH reactions

Proceedings of the Combustion Institute, 2016

Research paper thumbnail of Hollow-Cone Spray Modeling for Outwardly Opening Piezoelectric Injector

54th AIAA Aerospace Sciences Meeting, 2016

Research paper thumbnail of Physical and chemical effects of low octane gasoline fuels on compression ignition combustion

Research paper thumbnail of Ignition studies of n-heptane/iso-octane/toluene blends

Combustion and Flame, 2016

Research paper thumbnail of Ignition delay measurements of light naphtha: A fully blended low octane fuel

Proceedings of the Combustion Institute, 2016

Research paper thumbnail of Enhanced Transient Heat Transfer from Arrays of Jets Impinging on a Moving Plate

Research paper thumbnail of A blending rule for octane numbers of PRFs and TPRFs with ethanol

Research paper thumbnail of Effects of In-Cylinder Mixing on Low Octane Gasoline Compression Ignition Combustion

SAE Technical Paper Series, 2016

Research paper thumbnail of Modeling of Heating and Evaporation of FACE I Gasoline Fuel and its Surrogates

SAE Technical Paper Series, 2016

Research paper thumbnail of Spray Modeling for Outwardly-Opening Hollow-Cone Injector

SAE Technical Paper Series, 2016

Research paper thumbnail of Numerical Simulations of Hollow Cone Injection and Gasoline Compression Ignition Combustion With Naphtha Fuels

Volume 2: Emissions Control Systems; Instrumentation, Controls, and Hybrids; Numerical Simulation; Engine Design and Mechanical Development, 2015

Research paper thumbnail of Surrogate fuel formulation for light naphtha combustion in advanced combustion engines

Crude oil once recovered is further separated in to several distinct fractions to produce a range... more Crude oil once recovered is further separated in to several distinct fractions to produce a range of energy and chemical products. One of the less processed fractions is light naphtha (LN), hence they are more economical to produce than their gasoline and diesel counterparts. Recent efforts have demonstrated usage of LN as transportation fuel for internal combustion engines with slight modifications. In this study, a multicomponent surrogate fuel has been developed for light naphtha fuel using a multi-variable nonlinear constrained optimization scheme. The surrogate, consisting of palette species n-pentane, 2-methylhexane, 2-methylbutane, n-heptane and toluene, was validated against the LN using ignition quality tester following ASTM D6890 methodology. Comparison of LN and the surrogate fuel demonstrated satisfactory agreement.

Research paper thumbnail of Correction: A shock tube study of the branching ratios of propene + OH reaction

Phys. Chem. Chem. Phys., 2015

Correction for 'A shock tube stud... more Correction for 'A shock tube study of the branching ratios of propene + OH reaction' by Jihad Badra et al., Phys. Chem. Chem. Phys., 2015, 17, 2421-2431.

Research paper thumbnail of Enhanced Heat Transfer from Arrays of Jets Impinging on Plates

Multiple jets of various shapes, orientation and configuration are used regularly in a wide range... more Multiple jets of various shapes, orientation and configuration are used regularly in a wide range of engineering applications to provide heating or cooling with impingement on a plate being one of the most common configurations due to the improved heat transfer rates. Design optimization has largely relied on empirical correlations that are limited by the range over which they were originally generated. Computational Fluid Mechanics is now sufficiently advanced to be used as an alternative method for obtaining optimal designs. This project uses the commercial Fluent package to compute heat transfer from a bank of jets impinging on a plate. Results for a single jet are validated against experimental data. The use of advanced turbulence modeling and appropriate boundary layer formulations are key ingredients for obtaining reliable calculations. The heat transfer resulting form the use of multi-jet configurations will be discussed in the paper.

Research paper thumbnail of A methodology to relate octane numbers of binary and ternary n-heptane, iso-octane and toluene mixtures with simulated ignition delay times

Research paper thumbnail of Mixed butanols addition to gasoline surrogates: Shock tube ignition delay time measurements and chemical kinetic modeling

Combustion and Flame, 2015

Research paper thumbnail of Micro-mixer/combustor

A micro-mixer/combustor to mix fuel and oxidant streams into combustible mixtures where flames re... more A micro-mixer/combustor to mix fuel and oxidant streams into combustible mixtures where flames resulting from combustion of the mixture can be sustained inside its combustion chamber is provided. The present design is particularly suitable for diffusion flames. In various aspects the present design mixes the fuel and oxidant streams prior to entering a combustion chamber. The combustion chamber is designed to prevent excess pressure to build up within the combustion chamber, which build up can cause instabilities in the flame. A restriction in the inlet to the combustion chamber from the mixing chamber forces the incoming streams to converge while introducing minor pressure drop. In one or more aspects, heat from combustion products exhausted from the combustion chamber may be used to provide heat to at least one of fuel passing through the fuel inlet channel, oxidant passing through the oxidant inlet channel, the mixing chamber, or the combustion chamber. In one or more aspects, an...

Research paper thumbnail of Numerical Simulations of Heat Transfer from Arrays of Jets Impinging on a Plate

Research paper thumbnail of Characteristics of spray from a GDI fuel injector for naphtha and surrogate fuels

Research paper thumbnail of Chemical Kinetic Insights into the Octane Number and Octane Sensitivity of Gasoline Surrogate Mixtures

Research paper thumbnail of A shock tube study of C4–C6 straight chain alkenes + OH reactions

Proceedings of the Combustion Institute, 2016

Research paper thumbnail of Hollow-Cone Spray Modeling for Outwardly Opening Piezoelectric Injector

54th AIAA Aerospace Sciences Meeting, 2016

Research paper thumbnail of Physical and chemical effects of low octane gasoline fuels on compression ignition combustion

Research paper thumbnail of Ignition studies of n-heptane/iso-octane/toluene blends

Combustion and Flame, 2016

Research paper thumbnail of Ignition delay measurements of light naphtha: A fully blended low octane fuel

Proceedings of the Combustion Institute, 2016

Research paper thumbnail of Enhanced Transient Heat Transfer from Arrays of Jets Impinging on a Moving Plate

Research paper thumbnail of A blending rule for octane numbers of PRFs and TPRFs with ethanol

Research paper thumbnail of Effects of In-Cylinder Mixing on Low Octane Gasoline Compression Ignition Combustion

SAE Technical Paper Series, 2016

Research paper thumbnail of Modeling of Heating and Evaporation of FACE I Gasoline Fuel and its Surrogates

SAE Technical Paper Series, 2016

Research paper thumbnail of Spray Modeling for Outwardly-Opening Hollow-Cone Injector

SAE Technical Paper Series, 2016

Research paper thumbnail of Numerical Simulations of Hollow Cone Injection and Gasoline Compression Ignition Combustion With Naphtha Fuels

Volume 2: Emissions Control Systems; Instrumentation, Controls, and Hybrids; Numerical Simulation; Engine Design and Mechanical Development, 2015

Research paper thumbnail of Surrogate fuel formulation for light naphtha combustion in advanced combustion engines

Crude oil once recovered is further separated in to several distinct fractions to produce a range... more Crude oil once recovered is further separated in to several distinct fractions to produce a range of energy and chemical products. One of the less processed fractions is light naphtha (LN), hence they are more economical to produce than their gasoline and diesel counterparts. Recent efforts have demonstrated usage of LN as transportation fuel for internal combustion engines with slight modifications. In this study, a multicomponent surrogate fuel has been developed for light naphtha fuel using a multi-variable nonlinear constrained optimization scheme. The surrogate, consisting of palette species n-pentane, 2-methylhexane, 2-methylbutane, n-heptane and toluene, was validated against the LN using ignition quality tester following ASTM D6890 methodology. Comparison of LN and the surrogate fuel demonstrated satisfactory agreement.

Research paper thumbnail of Correction: A shock tube study of the branching ratios of propene + OH reaction

Phys. Chem. Chem. Phys., 2015

Correction for 'A shock tube stud... more Correction for 'A shock tube study of the branching ratios of propene + OH reaction' by Jihad Badra et al., Phys. Chem. Chem. Phys., 2015, 17, 2421-2431.

Research paper thumbnail of Enhanced Heat Transfer from Arrays of Jets Impinging on Plates

Multiple jets of various shapes, orientation and configuration are used regularly in a wide range... more Multiple jets of various shapes, orientation and configuration are used regularly in a wide range of engineering applications to provide heating or cooling with impingement on a plate being one of the most common configurations due to the improved heat transfer rates. Design optimization has largely relied on empirical correlations that are limited by the range over which they were originally generated. Computational Fluid Mechanics is now sufficiently advanced to be used as an alternative method for obtaining optimal designs. This project uses the commercial Fluent package to compute heat transfer from a bank of jets impinging on a plate. Results for a single jet are validated against experimental data. The use of advanced turbulence modeling and appropriate boundary layer formulations are key ingredients for obtaining reliable calculations. The heat transfer resulting form the use of multi-jet configurations will be discussed in the paper.

Research paper thumbnail of A methodology to relate octane numbers of binary and ternary n-heptane, iso-octane and toluene mixtures with simulated ignition delay times

Research paper thumbnail of Mixed butanols addition to gasoline surrogates: Shock tube ignition delay time measurements and chemical kinetic modeling

Combustion and Flame, 2015

Research paper thumbnail of Micro-mixer/combustor

A micro-mixer/combustor to mix fuel and oxidant streams into combustible mixtures where flames re... more A micro-mixer/combustor to mix fuel and oxidant streams into combustible mixtures where flames resulting from combustion of the mixture can be sustained inside its combustion chamber is provided. The present design is particularly suitable for diffusion flames. In various aspects the present design mixes the fuel and oxidant streams prior to entering a combustion chamber. The combustion chamber is designed to prevent excess pressure to build up within the combustion chamber, which build up can cause instabilities in the flame. A restriction in the inlet to the combustion chamber from the mixing chamber forces the incoming streams to converge while introducing minor pressure drop. In one or more aspects, heat from combustion products exhausted from the combustion chamber may be used to provide heat to at least one of fuel passing through the fuel inlet channel, oxidant passing through the oxidant inlet channel, the mixing chamber, or the combustion chamber. In one or more aspects, an...

Research paper thumbnail of Numerical Simulations of Heat Transfer from Arrays of Jets Impinging on a Plate

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