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
- On estimating physical and chemical properties of hydrocarbon fuels using mid-infrared FTIR spectra and regularized linear models
- A streamlined approach to hybrid-chemistry modeling for a low cetane-number alternative jet fuel
- 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 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
- Formulation of optimal surrogate descriptions of fuels considering sensitivities to experimental uncertainties
- Fuel effects on lean blow-out in a realistic gas turbine combustor
- A multi-wavelength speciation framework for high-temperature hydrocarbon pyrolysis
- A new method of estimating derived cetane number for hydrocarbon fuels
- 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
- Group contribution method for multicomponent evaluation with application to transportation fuels
- The role of preferential evaporation on the ignition of multicomponent fuels in a homogeneous spray/air mixture
- Large-Eddy Simulation of Fuel Effect on Lean Blow-out in Gas Turbines
- Shock Tube/Laser Absorption Measurements of the Pyrolysis of a Bimodal Test Fuel
- Ignition delay time correlations for distillate fuels
- SUAVE: An Open-Source Environment for Multi-Fidelity Conceptual Vehicle Design
- 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
- 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
- Species Time-History Measurements during Jet Fuel Pyrolysis
- Shock Tube Measurements of Species Time-Histories during Jet Fuel Pyrolysis and Oxidation
- Shock Tube Measurements of Jet and Rocket Fuels
- Reduced Order ODE Model for Linear Contrails
- The Effects of Rerouting Aircraft around the Arctic Circle on Arctic and Global Climate
- A Probabilistic Ice Habit Model for LES of Contrails
- Effects of plume-scale versus grid-scale treatment of aircraft exhaust photochemistry