All Stories

  1. Bayesian-Enhanced Low-Fidelity Correction Approach to Multifidelity Aerospace Design

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

    Prof. RAMANA V GRANDHI

  2. Status of Multifidelity Model Management Strategies in Aircraft Design

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

    Prof. RAMANA V GRANDHI

  3. High-Fidelity Aerodynamic Shape Optimization using Immersed Boundary Method

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

    Prof. RAMANA V GRANDHI

  4. A Nonlinear Finite Element Analysis Capability for the Optimization of Thermoelastic Structures

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

    Prof. RAMANA V GRANDHI

  5. Bayesian Low-Fidelity Correction Approach to Multi-Fidelity Aerospace Design

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

    Prof. RAMANA V GRANDHI

  6. Fatigue Life Optimization of Laser Peened Aircraft Components

    Article • October 2016, Bentham Science Publishers

    Prof. RAMANA V GRANDHI

  7. Prediction of Residual Stress Relaxation in Ti-6Al-4V subjected to Laser Peening

    Article • October 2016, Bentham Science Publishers

    Prof. RAMANA V GRANDHI

  8. Multi-Fidelity Design Optimization via Low-Fidelity Correction Technique

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

    Prof. RAMANA V GRANDHI

  9. A Robust Analytical Sensitivity Analysis for Coupled Aero-Structural Systems

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

    Prof. RAMANA V GRANDHI

  10. Multidisciplinary Design Optimization

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

    Prof. RAMANA V GRANDHI

  11. Impact of plasticity generated by Rayleigh waves on the residual stress behavior of structural components subjected to laser peening

    Article • International Journal of Structural Integrity, February 2015, Emerald

    Prof. RAMANA V GRANDHI

  12. Continuum Sensitivity Analysis for Structural Shape Design Variables Using Finite-Volume Method

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

    Prof. RAMANA V GRANDHI

  13. Nonlinear Aeroelastic Analysis of High Aspect-Ratio Wings Using Immersed Boundary Technique

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

    Prof. RAMANA V GRANDHI

  14. A Surrogate-based Adjustment Factor Approach to Multi-Fidelity Design Optimization

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

    Prof. RAMANA V GRANDHI

  15. Significance of Geometric Nonlinearity in the Design of Thermally Loaded Structures

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

    Prof. RAMANA V GRANDHI

  16. Response Surface Model Using the Sorted k-Fold Approach

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

    Prof. RAMANA V GRANDHI

  17. Topology Optimization of Thermoelastic Structures using Stress-based Design Criteria

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

    Prof. RAMANA V GRANDHI

  18. Aerodynamic Sensitivity Analysis based on Modified Navier-Stokes Equations

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

    Prof. RAMANA V GRANDHI

  19. Continuum Sensitivity Analysis for Structural Shape Design Variables Using Finite Volume Approach

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

    Prof. RAMANA V GRANDHI

  20. Utilizing an Adjustment Factor to Scale Between Multiple Fidelities Within a Design Process: A Stepping Stone to Dialable Fidelity Design

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

    Prof. RAMANA V GRANDHI

  21. A Response Surface Model Using the Sorted k-fold Approach

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

    Prof. RAMANA V GRANDHI