Stanford University
Projects
- Jet Noise Modeling and Measurements to Support Reduced LTO Noise of Supersonic Aircraft Technology Development
- Validation of Low-Exposure Noise Modeling by Open-Source Data Management and Visualization Systems Integrated with AEDT
- Aircraft Design and Performance Assessment Tool Enhancement
- National Jet Fuels Combustion Program – Area #5: Atomization Tests and Models
- National Jet Fuels Combustion Program – Area #4: Combustion Model Development and Evaluation
- National Jet Fuels Combustion Program – Area #2: Chemical Kinetics Model Development and Evaluation
- National Jet Fuels Combustion Program – Area #1: Chemical Kinetics Combustion Experiments
- Micro-Physical Modeling & Analysis of ACCESS 2 Aviation Exhaust Observations
- Aircraft Technology Modeling and Assessment
Lead Investigators
Publications
- A New Strategy of Characterizing Hydrocarbon Fuels Using FTIR Spectra and Generalized Linear Model with Grouped-Lasso Regularization
- Spectroscopic Inference of Alkane, Alkene, and Aromatic Formation During High-temperature JP8, JP5, and Jet-A Pyrolysis
- A Streamlined Approach to Hybrid-chemistry Modeling for a Low Cetane-number Alternative Jet Fuel
- On Estimating Physical and Chemical Properties of Hydrocarbon Fuels using Mid-infrared FTIR Spectra and Regularized Linear Models
- Multi-wavelength Speciation of High-temperature 1-butene Pyrolysis
- Kinetic Analysis of Distinct Product Generation in Oxidative Pyrolysis of Four Octane Isomers
- HOMO-LUMO Energy Splitting in Polycyclic Aromatic Hydrocarbons and Their Derivatives
- A Multi-wavelength Speciation Framework for High-temperature Hydrocarbon Pyrolysis
- A New Method of Estimating Derived Cetane Number for Hydrocarbon Fuels
- A Physics-based Approach to Modeling Real-fuel Combustion Chemistry–IV. HyChem Modeling of Combustion Kinetics of a Bio-derived Jet Fuel and its Blends with a Conventional Jet A
- A Shock Tube Study of Jet Fuel Pyrolysis and Ignition at Elevated Pressures and Temperatures
- A Physics-based Approach to Modeling Real-fuel Combustion Chemistry - I. Evidence from Experiments, and Thermodynamic, Chemical Kinetic and Statistical Considerations
- Large-Eddy Simulations of Fuel Effects on Gas Turbine Lean Blow-out
- Formulation of Optimal Surrogate Descriptions of Fuels Considering Sensitivities to Experimental Uncertainties
- Large-Eddy Simulation of Fuel Effect on Lean Blow-out in Gas Turbines
- Shock Tube Study of Jet Fuel Pyrolysis and Ignition at Elevated Pressure
- Evaluation of a Hybrid Chemistry Approach for Combustion of Blended Petroleum and Bio-derived Jet Fuels
- Combustion Kinetics of Conventional and Alternative Jet Fuels using a Chemistry (HyChem) Approach
- HyChem Model: Application to Petroleum-Derived Jet Fuels
- Evidence Supporting a Simplified Approach to Modeling High-Temperature Combustion Chemistry
- Fuel Effects on Lean Blow-out in a Realistic Gas Turbine Combustor
- The Role of Preferential Evaporation on the Ignition of Multicomponent Fuels in a Homogeneous Spray/Air Mixture
- Shock Tube/Laser Absorption Measurements of the Pyrolysis of a Bimodal Test Fuel
- Ignition Delay Time Correlations for Distillate Fuels
- Group Contribution Method for Multicomponent Evaluation with Application to Transportation Fuels
- Shock Tube Measurements of Jet and Rocket Fuels
- High-Fidelity Simulations of Fuel Injection and Atomization of a Hybrid Air-Blast Atomizer
- Effect of Aviation Fuel Type and Fuel Injection Conditions on Non-reacting Spray Characteristics of Hybrid Air Blast Fuel Injector
- Reduced Order ODE Model for Linear Contrails
- Shock Tube Measurements of Species Time-Histories during Jet Fuel Pyrolysis and Oxidation
- Species Time-History Measurements during Jet Fuel Pyrolysis
- SUAVE: An Open-Source Environment for Multi-Fidelity Conceptual Vehicle Design
- Effects of Plume-scale Versus Grid-scale Treatment of Aircraft Exhaust Photochemistry
- A Probabilistic Ice Habit Model for LES of Contrails
- The Effects of Rerouting Aircraft Around the Arctic Circle on Arctic and Global Climate