All Stories

  1. Towards Adjoint-based Sensitivity Analysis for Supersonic Jet Noise

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

    Research Engineer II Asitav Mishra, Enrico Fabiano

  2. ADGAR: A GPU Accelerated Adjoint Solver for Shape Optimization in Viscous Flows

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

    Research Engineer II Asitav Mishra

  3. Multiple-Fidelity Modeling of Interactional Aerodynamics

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

    Research Engineer II Asitav Mishra

  4. GPU Acceleration of a Discrete Adjoint solver for airfoil optimization.

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

    Research Engineer II Asitav Mishra

  5. Multiple Fidelity Modeling of Interactional Aerodynamics

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

    Research Engineer II Asitav Mishra

  6. Data-driven augmentation of turbulence models for adverse pressure gradient flows

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

    Research Engineer II Asitav Mishra

  7. An Efficient Parallel Overset Method for Aerodynamic Shape Optimization

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

    Ney Secco, Research Engineer II Asitav Mishra

  8. An unsteady coupled fluid-structure interactional adjoint-based optimization of flexible blades.

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

    Research Engineer II Asitav Mishra

  9. Time-dependent Aero-acoustic Adjoint-based Shape Optimization of Helicopter Rotors in Forward Flight

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

    Enrico Fabiano, Research Engineer II Asitav Mishra

  10. Coupled Aeroelastic Prediction of the Effects of Leading-Edge Slat on Rotor Performance

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

    Research Engineer II Asitav Mishra

  11. Time dependent adjoint-based optimization for coupled fluid–structure problems

    Article • Journal of Computational Physics, July 2015, Elsevier

    Research Engineer II Asitav Mishra

  12. Unsteady Aero-elastic Adjoint-based Aerodynamic Shape Optimization of Helicopter Rotors in Cruise

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

    Research Engineer II Asitav Mishra

  13. Helicopter Rotor Design using Adjoint-based Optimization in a Coupled CFD-CSD Framework

    Article • June 2013, American Institute of Aeronautics and Astronautics (AIAA)

    Research Engineer II Asitav Mishra

  14. Coupled CFD/CSD Prediction of the Effects of Trailing Edge Flaps on Rotorcraft Dynamic Stall Alleviation

    Article • January 2009, American Institute of Aeronautics and Astronautics (AIAA)

    Research Engineer II Asitav Mishra

  15. Computational Investigation of Trailing Edge Flap for Control of Vibration

    Article • June 2007, American Institute of Aeronautics and Astronautics (AIAA)

    Research Engineer II Asitav Mishra