All Stories

  1. Flamelet/Progress Variable Formulation with Pressure Variations for Modeling Rocket Combustion Dynamics

    Article • January 2024, American Institute of Aeronautics and Astronautics (AIAA)

    charles merkle, Timothy Weathers

  2. Investigations of Multi-Zonal Modeling Strategy for Rocket Combustion Dynamics

    Article • January 2024, American Institute of Aeronautics and Astronautics (AIAA)

    charles merkle

  3. Investigations and Improvement of Robustness of Reduced-Order Models of Reacting Flow

    Article • AIAA Journal, December 2019, American Institute of Aeronautics and Astronautics (AIAA)

    charles merkle

  4. Multifidelity Framework for Modeling Combustion Dynamics

    Article • AIAA Journal, February 2019, American Institute of Aeronautics and Astronautics (AIAA)

    charles merkle

  5. Investigations and Improvement of Robustness of Reduced-Order Models of Reacting Flow

    Article • January 2019, American Institute of Aeronautics and Astronautics (AIAA)

    charles merkle

  6. Exploration of POD-Galerkin Techniques for Developing Reduced Order Models of Nonlinear Euler Equations

    Article • January 2017, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. Cheng Huang, charles merkle

  7. Exploration of POD-Galerkin Techniques for Developing Combustion Response Functions

    Article • July 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. Cheng Huang, charles merkle

  8. Exploration of POD-Galerkin Techniques for Developing Reduced Order Models of the Euler Equations

    Article • January 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. Cheng Huang, charles merkle

  9. Response Function Modeling in the Study of Longitudinal Combustion Instability by a Quasi-1D Eulerian Solver

    Article • July 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Francesco Nasuti, Dr. Cheng Huang, Maria Luisa Frezzotti, charles merkle

  10. Determination of Heat Release Response Function from 2D Hybrid RANS-LES Data for the CVRC Combustor

    Article • July 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Francesco Nasuti, Dr. Cheng Huang, Maria Luisa Frezzotti, charles merkle

  11. Global POD-Based Adaption Scheme for Reduced Order Models of the Reaction-Advection Equation

    Article • July 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. Cheng Huang, charles merkle

  12. Advected Upstream Splitting Method for the Coupled Maxwell and Navier–Stokes Equations

    Article • AIAA Journal, March 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. Trevor M. Moeller, Dr Richard J Thompson, charles merkle

  13. Comparison of Artificial Dissipation and Filtering Schemes for Time-Accurate Simulations

    Article • January 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Ann Karagozian, charles merkle

  14. Fundamental Physics and Model Assumptions in Turbulent Combustion Models for Aerospace Propulsion

    Article • July 2014, American Institute of Aeronautics and Astronautics (AIAA)

    charles merkle

  15. Exploration of POD-Galerkin Method in Developing a Flame Model for Combustion Instability Problems

    Article • June 2014, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. Cheng Huang, charles merkle

  16. A Unified Hyperbolic Model for Coupled Fluid Dynamics and Electromagnetics in Aerospace Applications

    Article • January 2014, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Richard J Thompson, Dr. Trevor M. Moeller, charles merkle

  17. An Approximate Riemann Solver for Relativistic Two-fluid Plasmadynamics

    Article • January 2014, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Richard J Thompson, Dr. Trevor M. Moeller, charles merkle