# overview
Fluid and gas dynamics, numerical modeling,  combustion, plasma discharges, plasma assisted ignition and combustion, turbulence.

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4012 Fluid Mechanics And Thermal Engineering

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5102 Atomic, Molecular And Optical Physics

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Subsurface detection and discrimination of buried objects group using remote sensing technique

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Institute of Electrical and Electronics Engineers (IEEE)

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Effects of the Laser Intensity Profile on Ignition of Hydrogen-Air Mixture

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American Institute of Aeronautics and Astronautics (AIAA)

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Beam Shaping for the Laser Energy Deposition in Air

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American Institute of Aeronautics and Astronautics (AIAA)

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Limitations on High-Spatial Resolution Measurements of Turbulence Using Femtosecond Laser Tagging

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American Institute of Aeronautics and Astronautics (AIAA)

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Ignition System Based on the Nanosecond Pulsed Discharge

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Institute of Electrical and Electronics Engineers (IEEE)

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On the effect of nonequilibrium plasma on the minimum ignition energy: Part 2

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Self-consistent model and numerical approach for laser-induced non-equilibrium plasma

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Dual-pulse laser energy deposition for the flow control in a supersonic flow

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American Institute of Aeronautics and Astronautics (AIAA)

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Microwave-Assisted Flame With Sodium Seeding

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Institute of Electrical and Electronics Engineers (IEEE)

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Refractive index of nitrogen in thermochemical nonequilibrium

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American Institute of Aeronautics and Astronautics (AIAA)

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Modeling of Nonequilibrium Air Plasma Generation by Transversal Gas Discharge

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Institute of Electrical and Electronics Engineers (IEEE)

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Dynamics of dual-pulse laser energy deposition in a supersonic flow

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Parametrical study of aero-optical effects using shell models of turbulence

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American Institute of Aeronautics and Astronautics (AIAA)

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Quantification of plasma enabled surface cooling by electron emission from high temperature materials

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Femtosecond laser discharge and small scale turbulence

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American Institute of Aeronautics and Astronautics (AIAA)

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Comparative Analysis of Engine Ignition Systems

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Institute of Electrical and Electronics Engineers (IEEE)

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Charge-Formation Processes in Liquid Dielectrics

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Computational fluid dynamic model of electron transpiration cooling in weakly ionized air flows

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American Institute of Aeronautics and Astronautics (AIAA)

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Cesium seeding for effective electron transpiration cooling in hypersonic flows

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Nonequilibrium effects in high-speed flow: experiment and simulation

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American Institute of Aeronautics and Astronautics (AIAA)

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Isentropic plasma sheath model for improved fidelity

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Deflagration to detonation transition assisted by equilibrium and non-equilibrium plasma

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Ignition by Short Duration, Nonequilibrium Plasma: Basic Concepts and Applications in Internal Combustion Engines

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Modeling studies of electron transpiration cooling at high-speed flows.

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American Institute of Aeronautics and Astronautics (AIAA)

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Aero-optical effects in non-equilibrium air

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American Institute of Aeronautics and Astronautics (AIAA)

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Nanosecond Pulsed Discharge Igniter for Internal Combustion Engines

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Turbulent cascade process in arc driven plasma channels

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Mathematical modeling of dual-pulse laser ignition in a turbulent flow

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American Institute of Aeronautics and Astronautics (AIAA)

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Numerical analysis of the non-steady discharge characteristics in the plasmatron channel

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Deflagration to detonation transition assisted by equilibrium and non-equilibrium plasma

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American Institute of Aeronautics and Astronautics (AIAA)

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Sheath layer effects on electron transpiration cooling

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American Institute of Aeronautics and Astronautics (AIAA)

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Plasma sheath models for electron transpiration cooling in hypersonic vehicles

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American Institute of Aeronautics and Astronautics (AIAA)

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Effect of Plasma on the Deflagration to Detonation Transition

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Investigation of Non-Self-Maintained Gas Discharge in Propane-Air Mixture

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Modeling of laser ignition in hydrogen-air mixture

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American Institute of Aeronautics and Astronautics (AIAA)

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Ignition Delay Time and Laminar Flame Velocity for a Combined Laser-Microwave Ignition

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Institute of Electrical and Electronics Engineers (IEEE)

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Institute of Electrical and Electronics Engineers (IEEE)

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Numerical analysis and prediction of Aero-optical effects

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American Institute of Aeronautics and Astronautics (AIAA)

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American Institute of Aeronautics and Astronautics (AIAA)

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Numerical Study of Laser-Induced Ignition at high speed flows

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American Institute of Aeronautics and Astronautics (AIAA)

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Combustion Dynamics of Microwave Enhanced Flame

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American Institute of Aeronautics and Astronautics (AIAA)

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Turbulent Cascade Process in Arc Driven Plasma Channels

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American Institute of Aeronautics and Astronautics (AIAA)

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Numerical modeling of laser energy deposition for supersonic flow control

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Correction: Dual-pulse laser energy deposition for the flow control in a supersonic flow

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American Institute of Aeronautics and Astronautics (AIAA)

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Dynamics of a Laser-Induced Filament Supported and Controlled by a Direct Current Discharge

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American Institute of Aeronautics and Astronautics (AIAA)

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2018 PLASMADYNAMICS AND LASERS CONFERENCE

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Methane-Air Mixture Ignition by Combined Laser and Microwave Discharges

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American Institute of Aeronautics and Astronautics (AIAA)

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Numerical Modeling of Laser Heating and Evaporation of a Single Droplet

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Magnetized radio-frequency sheath in low temperature plasma

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American Institute of Aeronautics and Astronautics (AIAA)

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Pulsed Power Science and Technology Temporal Analysis of Exploding Film Burst Phenomenon.................................................... TM DiSanto, S. Olabisi, DP Muffoletto, KM Burke, HL Moore, Jr., H. Singh, and JL Zirnheld 603 Other Topics in Plasma Science Improvement on Stability of Water Arcjet......................... L. Hou, Y. Shen, H. Tang, and W. Zhao 608

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Plasma defocusing in dual-pulse laser ignition

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On the effect of nonequilibrium plasma on the minimum ignition energyPart 1: Discharge model

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Two-dimensional non-equilibrium plasma model for dual-pulse laser ignition

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Space and time analysis of the N2 vibrational non-equilibrium in the N2 and air nanosecond discharge afterglow

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American Institute of Aeronautics and Astronautics (AIAA)

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MODELING OF NONEQUILIBRIUM PLASMA ASSISTED COMBUSTION

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Collisional plasma sheath effects on thermionic electron emission

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American Institute of Aeronautics and Astronautics (AIAA)

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Correction: Deflagration to detonation transition assisted by equilibrium and non-equilibrium plasma

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American Institute of Aeronautics and Astronautics (AIAA)

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Influence of vibrational non-equilibrium on the polarizability and refraction index in air: computational study

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Mathematical Model of Dual-Pulse Laser Ignition

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American Institute of Aeronautics and Astronautics (AIAA)

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On the Effect of Nonequilibrium Plasma on the Minimum Ignition Energy: Part 2

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Institute of Electrical and Electronics Engineers (IEEE)

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Influence of turbulent pulsations on the deviation from ionization equilibrium

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American Institute of Aeronautics and Astronautics (AIAA)

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Nanosecond pulsed discharge in a water vapor

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American Institute of Aeronautics and Astronautics (AIAA)

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High Temperature Nonequilibrium Effects on Atomic and Molecular Polarizability

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Vorticity Generation with Defocusing Effect for Dual-Pulse Laser Plasma in Air

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Laser induced plasma in hydrogen-air mixtures.

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Measurements of N2 refractive index and scalar polarizability in a pulsed nanosecond non-equilibrium discharge by Mach-Zehnder interferometry and spontaneous Raman scattering

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Fluid Modelling of Plasma Sheaths with Thermionically Emitted Electrons

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ADVANCED IGNITION SYSTEM FOR INTERNAL COMBUSTION ENGINES

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Simulation of the non-equilibrium transverse arc discharge in air

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Improvement of the Gas Turbine Plasma Assisted Combustor Characteristics

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American Institute of Aeronautics and Astronautics (AIAA)

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Three-dimensional Effects in Dual-pulse Laser Energy Deposition

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American Institute of Aeronautics and Astronautics (AIAA)

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Study of electron transpiration cooling under rapid laser heat flux modulation

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

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On the Effect of Nonequilibrium Plasma on the Minimum Ignition EnergyPart 1: Discharge Model

# publications[].publisher
Institute of Electrical and Electronics Engineers (IEEE)

# streetAddress
Texas A&M University; Aerospace Engineering; 3141 TAMU