All Stories

  1. Removal of Spurious Noise From Permeable FWH Data Surfaces

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

    Mehdi R. Khorrami

  2. Aeroacoustic Computations of a Transonic Truss-Braced Wing Aircraft: Part 2 – Acoustic Signature and Noise Source Identification

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

    Mehdi R. Khorrami

  3. Aeroacoustic Computations of a Transonic Truss-Braced Wing Aircraft: Part 1 – Aerodynamic and Airframe Noise Simulations

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

    Mehdi R. Khorrami

  4. Effects of Porous Gap Fillers on Leading-Edge Slat Noise of 30P30N. Part II: PIV Measurements

    Article • June 2022, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. Meelan Choudhari, kyle pascioni, Mehdi R. Khorrami, Dr. Travis Turner

  5. Effects of Porous Gap Fillers on 30P30N Leading-Edge Slat Noise. Part I: Surface Pressure and Acoustics

    Article • June 2022, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. Meelan Choudhari, kyle pascioni, Mehdi R. Khorrami, Dr. Travis Turner

  6. Slat Noise Control Using a Slat Gap Filler

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

    kyle pascioni, Mehdi R. Khorrami, Dr. Travis Turner, Dr. Meelan Choudhari

  7. Optical Geolocation for small Unmanned Aerial System

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

    Mehdi R. Khorrami

  8. Comparison of Measured and Simulated Acoustic Signatures for a Full-Scale Aircraft with and without Airframe Noise Abatement

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

    Mehdi R. Khorrami

  9. Flight-Test Evaluation of Airframe Noise Mitigation Technologies

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

    Mehdi R. Khorrami

  10. Evaluation of Methods for In-Situ Calibration of Field-Deployable Microphone Phased Arrays

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

    Mehdi R. Khorrami

  11. On the Importance of Spatial Resolution for Flap Side Edge Noise Prediction

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

    Mehdi R. Khorrami

  12. A Comparative Study of Simulated and Measured Main Landing Gear Noise for Large Civil Transports

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

    Mehdi R. Khorrami

  13. Aeroacoustic Simulations of a Nose Landing Gear with FUN3D: A Grid Refinement Study

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

    Mehdi R. Khorrami

  14. Computational Evaluation of Airframe Noise Reduction Concepts at Full Scale

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

    Andreas Hazir, Mehdi R. Khorrami

  15. Acoustic Measurements of a Large Civil Transport Main Landing Gear Model

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

    Mehdi R. Khorrami

  16. Development and Calibration of a Field-Deployable Microphone Phased Array for Propulsion and Airframe Noise Flyover Measurements

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

    Mehdi R. Khorrami

  17. Airframe Noise Prediction of a Full Aircraft in Model and Full Scale Using a Lattice Boltzmann Approach

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

    Mehdi R. Khorrami

  18. Simulation-Based Airframe Noise Prediction of a Full-Scale, Full Aircraft

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

    Mehdi R. Khorrami

  19. An Assessment of Flap and Main Landing Gear Noise Abatement Concepts

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

    Mehdi R. Khorrami

  20. Evaluation of Airframe Noise Reduction Concepts via Simulations Using a Lattice Boltzmann Approach

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

    Dr Damiano Casalino, Mehdi R. Khorrami

  21. A Comparative Study of Simulated and measured Gear-Flap Flow Interaction

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

    Mehdi R. Khorrami

  22. Comparison of Computational and Experimental Microphone Array Results for an 18%-Scale Aircraft Model

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

    Dr Damiano Casalino, Mehdi R. Khorrami

  23. Characterization of Flap Edge Noise Radiation from a High-Fidelity Airframe Model

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

    Dr Christopher J Bahr, Mehdi R. Khorrami

  24. Flap Side-Edge Vortex Dynamics

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

    Dr Damiano Casalino, Andreas Hazir, Mehdi R. Khorrami

  25. Aeroacoustic Simulations of a Nose Landing Gear using FUN3D on Pointwise Unstructured Grids

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

    Mehdi R. Khorrami

  26. Aerodynamic Measurements of a Gulfstream Aircraft Model With and Without Noise Reduction Concepts

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

    Mehdi R. Khorrami

  27. Aeroacoustic Evaluation of Flap and Landing Gear Noise Reduction Concepts

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

    Mehdi R. Khorrami

  28. Flow-Field Investigation of Gear-Flap Interaction on a Gulfstream Aircraft Model

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

    Mehdi R. Khorrami

  29. Towards Full Aircraft Airframe Noise Prediction: Detached Eddy Simulations

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

    Mehdi R. Khorrami

  30. Towards Full Aircraft Airframe Noise Prediction: Lattice Boltzmann Simulations

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

    Dr Damiano Casalino, Mehdi R. Khorrami