All Stories

  1. Reduced-Order Modeling of Resolved Turbulent Flows for High-Speed Fluid-Structure Interaction Analysis

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

    Peretz Friedmann

  2. Evaluation of Shock Wave-Boundary Layer Interaction Modeling Capabilities for Use in a Hypersonic Aerothermoelastic Framework

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

    Peretz Friedmann

  3. Vibration Reduction on Helicopter Rotors Using Open Loop Flow Control

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

    Ryan Patterson, Peretz Friedmann

  4. Helicopter Shipboard Landing Simulation Including Wind, Deck Motion and Dynamic Ground Effect

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

    Peretz Friedmann, Abhinav Sharma

  5. Multi-Objective Optimization Framework for Hypersonic Aerothermoelastic Scaling Laws and Its Application

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

    Peretz Friedmann

  6. Aerothermoelastic Scaling Laws for Hypersonic Skin Panel Configurations with Arbitrary Flow Orientation

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

    Peretz Friedmann

  7. Application of a CFD-Based Surrogate Approach for Active Flow Control Modeling

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

    Peretz Friedmann, Ryan Patterson

  8. A Surrogate-Based Optimization Framework for Hypersonic Aerothermoelastic Scaling Laws with Application to Skin Panels

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

    Peretz Friedmann

  9. Simulation of Maritime Helicopter Dynamics During Approach to Landing With Time-Accurate Wind-Over-Deck

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

    Peretz Friedmann, Abhinav Sharma

  10. Integrated Aerothermoelastic Analysis Framework with Application to Skin Panels

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

    Peretz Friedmann

  11. Multifidelity coKriging for High-Dimensional Output Functions with Application to Hypersonic Airloads Computation

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

    Peretz Friedmann

  12. Robust Design of Small Unmanned Helicopter for Hover Performance Using Taguchi Method

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

    Peretz Friedmann

  13. Application of Vortex Methods to Coaxial Rotor Wake and Load Calculations in Hover

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

    Peretz Friedmann, Puneet Singh

  14. Active and Passive Helicopter Noise Reduction Using the AVINOR/HELINOIR Code Suite

    Article • Journal of Aircraft, September 2017, American Institute of Aeronautics and Astronautics (AIAA)

    Peretz Friedmann

  15. An Aerothermoelastic Analysis Framework Enhanced by Model Order Reduction With Applications

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

    Peretz Friedmann

  16. The HELINOIR Aeroacoustic Code and its Application to Active/Passive Helicopter Noise Reduction

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

    Peretz Friedmann

  17. Application of Vortex Methods to Coaxial Rotor Wake and Load Calculations

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

    Puneet Singh, Peretz Friedmann

  18. Robust Design of Small-Scale Unmanned Helicopter for Hover Performance using Taguchi Method

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

    Peretz Friedmann

  19. Comprehensive Numerical Assessment of Rotorcraft Vibration and Noise Control Using Microflaps

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

    Peretz Friedmann

  20. Forced and Aeroelastic Responses of Bird-Damaged Fan Blades: A Comparison and Its Implications

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

    Peretz Friedmann

  21. An Integrated Aerothermoelastic Analysis Framework for Predicting the Response of Composite Panels

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

    Peretz Friedmann

  22. Forced and Aeroelastic Response of Bird-Damaged Fan Blades - A Comparison and Its Implications

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

    Peretz Friedmann

  23. Uncertainty Propagation in Integrated Airframe–Propulsion System Analysis for Hypersonic Vehicles

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

    Peretz Friedmann

  24. Optimization of Flexible Flapping-Wing Kinematics in Hover

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

    Peretz Friedmann

  25. Hypersonic Aeroelastic and Aerothermoelastic Studies Using Computational Fluid Dynamics

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

    Peretz Friedmann

  26. Aeroelastic Response of Bird-Damaged Fan Blades Using a Coupled CFD/CSD Framework

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

    Peretz Friedmann