All Stories

  1. Sonic Boom Ground Noise Minimization via the Adjoint Method

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

    Dr. David L Rodriguez, Sriram Rallabhandi

  2. Discretization Error Estimation and Control for Farfield Acoustic Signatures

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

    Sriram Rallabhandi

  3. Goal-Oriented Discretization Error Control in Coupled Nearfield-Farfield Low-Boom Simulations

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

    Sriram Rallabhandi, Dr. David L Rodriguez

  4. Propagation Analysis Using sBOOM for the Third AIAA Sonic Boom Prediction Workshop

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

    Sriram Rallabhandi

  5. Propagation Analysis of the 3rd Sonic Boom Prediction Workshop Cases using sBOOM

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

    Sriram Rallabhandi

  6. Summary of Propagation Cases of the Third AIAA Sonic Boom Prediction Workshop

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

    Sriram Rallabhandi

  7. Adjoint-Based Design of a Distributed Propulsion Concept with a Power Objective

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

    Sriram Rallabhandi

  8. Application of Exactly Linearized Error Transport Equations to Sonic Boom Prediction Workshop

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

    Sriram Rallabhandi

  9. Summary of Propagation Cases of the Second AIAA Sonic Boom Prediction Workshop

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

    Sriram Rallabhandi

  10. Sonic Boom Prediction and Mitigation using Three-Dimensional Earth Effects

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

    Sriram Rallabhandi

  11. Mitigation of Engine Inlet Distortion through Adjoint-Based Design

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

    Sriram Rallabhandi

  12. Propagation Summary of the Second AIAA Sonic Boom Prediction Workshop

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

    Sriram Rallabhandi

  13. Adjoint-Based Mesh Adaptation for the Sonic Boom Signature Loudness

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

    Sriram Rallabhandi

  14. Viscous Aerodynamic Shape Optimization with Installed Propulsion Effects

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

    Sriram Rallabhandi

  15. Impact of Aeroelastic Uncertainties on Sonic Boom Signature of a Commercial Supersonic Transport Configuration

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

    Prof. Melike Nikbay, Sriram Rallabhandi

  16. Uncertainty Analysis and Robust Design of Low-Boom Concepts Using Atmospheric Adjoints

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

    Sriram Rallabhandi

  17. Inlet Trade Study for a Low-Boom Aircraft Demonstrator

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

    Sriram Rallabhandi

  18. Inlet Trade Study for a Low Boom Aircraft Demonstrator

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

    Sriram Rallabhandi

  19. Full-Carpet Design of a Low-Boom Demonstrator Concept

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

    Sriram Rallabhandi

  20. Uncertainty Analysis and Robust Design of Low-Boom Concepts using Atmospheric Adjoints

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

    Sriram Rallabhandi

  21. Application of Adjoint Methodology to Supersonic Aircraft Design Using Reversed Equivalent Areas

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

    Sriram Rallabhandi

  22. Application of adjoint methodology in various aspects of sonic boom design

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

    Sriram Rallabhandi