All Stories

  1. Exploration of Reduced-Order Models for Rocket Combustion Applications

    Article • January 2018, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. Cheng Huang

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

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

    Dr. Cheng Huang

  3. Development and Application of an Energy Balance Analysis for Combustion

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

    Dr. Cheng Huang, Dr Swanand Sardeshmukh

  4. Extraction of response function from numerical simulations and their use for longitudinal combustion intsbility modeling

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

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

  5. 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

  6. Analysis of Self-Excited Combustion Instabilities Using Decomposition Techniques

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

    Dr. Cheng Huang

  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. Approaches for Comparing Numerical Simulation of Combustion Instability and Flame Imaging

    Article • Journal of Propulsion and Power, March 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. Cheng Huang

  9. Impact of Chemical Kinetics Mechanisms on the Predictions of Bluff Body Stabilized Flames

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

    Dr. Cheng Huang, Dr Swanand Sardeshmukh

  10. Modeling and Simulation of Bluff Body Stabilized Turbulent Premixed Flames

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

    Dr. Cheng Huang, Dr. Brent A Rankin

  11. Flamelet Modeling Studies of a Continuously Variable Resonance Combustor

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

    Dr. Cheng Huang, Dr Swanand Sardeshmukh

  12. 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

  13. 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

  14. 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

  15. 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

  16. Concurrent Experimental and Computational Study of Combustion Dynamics in a Single-Element Lean Direct Injection (LDI) Gas Turbine Combustor

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

    Dr. Cheng Huang

  17. Effects of Physical Modeling on Combustion Instability Predictions in a Single-Element Lean Direct Injection Gas Turbine Combustor

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

    Dr. Cheng Huang

  18. Combustion Dynamics Behavior in a Single-Element Lean Direct Injection (LDI) Gas Turbine Combustor

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

    Dr. Cheng Huang

  19. Development of Validation Approaches for Numerical Simulation of Combustion Instability using Flame Imaging

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

    Dr. Cheng Huang

  20. 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

  21. A Parametric Study of Combustion Dynamics in a Single-Element Lean Direct Injection Gas Turbine Combustor: Part II: Experimental Investigation

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

    Dr. Cheng Huang

  22. Computational Study of Combustion Dynamics in a Single-Element Lean Direct Injection Gas Turbine Combustor

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

    Dr. Cheng Huang