All Stories

  1. Performance of Flamelet Models with Epsilon Tracking for Diffusion Flame Simulations

    Article • January 2026, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. Feng Liu

  2. Flamelet Model with Epsilon Tracking in a Turbine Stator

    Article • January 2026, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. Feng Liu

  3. A train of burst vortices and a coexisting large cumulative vortex induced by a single-dielectric-barrier-discharge plasma actuator in burst mode

    Article • Physics of Fluids, August 2025, American Institute of Physics

    Dr. Feng Liu

  4. Bifurcation paths and stability of non-unique solutions of the axisymmetric Lamb–Oseen vortex in a pipe of finite-length

    Article • Physics of Fluids, June 2025, American Institute of Physics

    Dr. Feng Liu

  5. Large-Eddy Simulation of Reacting Flow in a Turbine Stage

    Article • January 2025, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. Feng Liu

  6. Simulation of Multi-Injector H2-O2Rocket Combustion Instability

    Article • January 2025, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. Feng Liu

  7. Development of a Pressure-Based Solution Method for Dense Gas Flow

    Article • January 2025, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. Feng Liu

  8. ANN Models for Prediction of Thermodynamic Properties in Dense Gas Flow

    Article • January 2025, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. Feng Liu

  9. Thermal effect on the flow induced by a single-dielectric-barrier-discharge plasma actuator under steady actuation

    Article • Physics of Fluids, September 2024, American Institute of Physics

    Dr. Feng Liu

  10. Numerical Investigation of Diffusion Flame in Transonic Flow with Large Pressure Gradient

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

    Dr. Feng Liu

  11. Turbulent Accelerating Combusting Flows with a Methane-Vitiated Air Flamelet Model

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

    Dr. Feng Liu

  12. Machine-Learning Models for Loss and Deviation Angle of Compressor Cascades

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

    Dr. Feng Liu

  13. Design Optimization of Multi-Stage Axial-Flow Compressor Using Machine Learning Models

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

    Dr. Feng Liu

  14. Flow induced by a pair of plasma actuators on a circular cylinder in still air under duty-cycle actuation

    Article • Physics of Fluids, December 2022, American Institute of Physics

    Dr. Feng Liu

  15. Numerical simulation of the flow around a square cylinder under plasma actuator control

    Article • Physics of Fluids, December 2021, American Institute of Physics

    Dr. Feng Liu

  16. Simulation of flow induced by single-dielectric-barrier-discharge plasma actuator using a high-order flux-reconstruction scheme

    Article • Physics of Fluids, April 2021, American Institute of Physics

    Dr. Feng Liu

  17. Implicit Time-Spectral Method for Unsteady Reynolds-Averaged Navier–Stokes Computations of Turbulent Flows

    Article • AIAA Journal, January 2021, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. Feng Liu, Dr. Lei Zhan

  18. Non-classical Isentropic Flow Behavior of a Bethe-Zel' dovich-Thompson Gas

    Article • January 2021, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. Feng Liu, Jingyi Zeng

  19. Optimal Tolerance Allocation in Blade Manufacturing by Sensitivity-Based Performance Impact Evaluation

    Article • Journal of Propulsion and Power, July 2020, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. Feng Liu

  20. Vortices Induced by a Dielectric Barrier Discharge Plasma Actuator Under Burst-Mode Actuation

    Article • AIAA Journal, June 2020, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. Feng Liu

  21. Nonlinear Combustion Instability in a Multi-Injector Rocket Engine

    Article • AIAA Journal, January 2020, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. Feng Liu, Taylor Morgan

  22. Wing Flutter Prediction by a Small-Disturbance Euler Method on Body-Fitted Curvilinear Grids

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

    Dr. Feng Liu

  23. Simulation of NACA0015 flow separation control by burst-mode plasma actuation

    Article • Physics of Plasmas, June 2019, American Institute of Physics

    Dr. Feng Liu, Borui Zheng

  24. Body Force Calculation of Steady-State Plasma Flow with Accurate Pressure Measurement

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

    Dr. Feng Liu

  25. On the Accuracy of Harmonic Methods and a New Similarity Rule for Unsteady Transonic Flow

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

    Dr. Feng Liu

  26. Resonance Prediction and the Limitations for Linear Methods

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

    Dr. Feng Liu

  27. Vorticity Dynamics and Flow Statistics Near the Edge of High-Speed Multi-Stream Jets

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

    Dr. Feng Liu

  28. Parametric study of burst mode on vortex structure induced by DBD plasma actuator

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

    Dr. Feng Liu

  29. Unsteady Flow Characteristics of a Double-side Sliding Pulsed Discharge Plasma Actuation

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

    Borui Zheng, Dr. Feng Liu

  30. Fully Implicit Chebyshev Time-Spectral Method for General Unsteady Flows

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

    Dr. Feng Liu, Dr. Lei Zhan

  31. Diesel, Spark-Ignition, and Turboprop Engines for Long-Duration Unmanned Air Flights

    Article • Journal of Propulsion and Power, July 2018, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. Feng Liu

  32. Performance Impact of Manufacturing Variations for Multistage Steam Turbines

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

    Dr. Feng Liu, Jiaqi Luo

  33. Unsteady Navier-Stokes Computations on GPU Architectures

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

    Ferran Marti , Dr. Feng Liu

  34. Flutter Study of NACA 64A010 Airfoil Using URANS and e^N Transition Models Coupled with an Integral Boundary Layer Code

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

    Dr. Feng Liu, Ferran Marti

  35. Multiple Equilibrium Points of Airfoil Flutter in Viscous Flow

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

    Dr. Feng Liu, Ferran Marti

  36. Flow Simulations of The Dynamics of a Perturbed Solid-Body Rotation Flow

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

    Prof Zvi Rusak, Dr. Feng Liu

  37. An experimental and numerical study of laminar separation on elliptic airfoil at low Reynolds numbers

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

    Dr. Feng Liu, Xuanshi Meng

  38. Optimization of Dielectric Barrier Discharge Plasma Actuators for Conical-Forebody Flow Control

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

    Dr. Feng Liu, Xuanshi Meng

  39. Simulation of Body Force Effect on Steady and Unsteady Flow Induced by DBD Plasma Actuator

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

    Dr. Feng Liu

  40. Separation Control Using Plasma Actuator on an Elliptic Airfoil at Low Reynolds Numbers

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

    Dr. Feng Liu, Xuanshi Meng

  41. Conical Forebody Flow Control Using Thick Dielectric Barrier Plasma Actuators

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

    Dr. Feng Liu, Xuanshi Meng

  42. PIV-Estimated DBD Plasma-Actuator Thrust Verified by Measurement in Quiescent Air

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

    Dr. Feng Liu

  43. Quiet Nozzle Concepts for Three-Stream Jets

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

    Dr. Feng Liu

  44. Pressure Characteristics over 20 deg Cone Forebody at Alpha 35 deg and Re (0.1-0.9)×106

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

    Dr. Feng Liu, Xuanshi Meng

  45. Laminar-Separation-Bubbles Flow Control over Airfoil Using SDBD Plasma Actuator

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

    Dr. Feng Liu

  46. Phase-Locked Schlieren of Periodic Nanosecond-Pulsed DBD Actuation in Quiescent Air

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

    Dr. Feng Liu, Xuanshi Meng

  47. Nanosecond-SDBD Actuation over a Conical Forebody at Wind Speed 72 m/s and Angle of Attack 45 degree

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

    Dr. Feng Liu, Xuanshi Meng

  48. Pressure Investigations over a Conical Forebody under Duty-Cycled Plasma Actuations

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

    Dr. Feng Liu, Xuanshi Meng

  49. CFD Validation of PIV-based Estimation of DBD Plasma-Actuation Force

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

    Dr. Feng Liu

  50. Effect of Voltage and Frequency on Starting Repetitive Nanosecond Pulsed DBD

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

    Dr. Feng Liu, Xuanshi Meng

  51. Plasma Laminar-Separation-Bubble Control over Airfoil at Low Reynolds Numbers

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

    Dr. Feng Liu, Xuanshi Meng

  52. Pressures over a Conical Forebody under Repetitive Nanosecond Pulse SDBD Actuations

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

    Dr. Feng Liu, Xuanshi Meng

  53. Starting Flow by Repetitive Nanosecond Pulsed DBD Actuation at Microseconds and Milliseconds in Quiescent Air

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

    Dr. Feng Liu, Xuanshi Meng

  54. Endwall contouring, optimization, adjoint

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

    Jiaqi Luo, Dr. Feng Liu

  55. Towards a Low-Cost Wavepacket Model of the Jet Noise Source

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

    Dr. Feng Liu

  56. Computational Analysis of Conical Forebody Flow at High Alpha with Transitional Model

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

    Dr. Feng Liu, Borui Zheng

  57. Reduction of Radiation Efficiency in High-Speed Jets

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

    Dr. Feng Liu

  58. Comparison of Pressures Driven by Repetitive Nanosecond Pulses to AC Result

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

    Dr. Feng Liu

  59. Establishment of Mapping Relationship between Plasma Actuator Parameters and Body Force based on Neural Networks

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

    Dr. Feng Liu, Borui Zheng

  60. Comparison of Velocities Driven by Repetitive Nanosecond Pulses to AC Result

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

    Dr. Feng Liu, Xuanshi Meng

  61. Flow Control over a Conical Forebody Using Pulsed Nanosecond Discharge Actuators

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

    Dr. Feng Liu