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  1. Propagation of Three-Dimensional Disturbances Over Finite Wings

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

    Dr Shahid Mughal

  2. Open-source framework for transonic boundary layer natural transition analysis over complex geometries in Nektar++

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

    Dr Shahid Mughal, Ganlin Lyu

  3. An adjoint compressible linearised Navier–Stokes approach to model generation of Tollmien–Schlichting waves by sound

    Article • Journal of Fluid Mechanics, August 2019, Cambridge University Press

    Dr Shahid Mughal

  4. Aerodynamic and Transition Analysis of the Hybrid Laminar Flow ControlWing at ARA Wind Tunnel

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

    Dr Shahid Mughal

  5. Global Stability Analysis of a Boundary Layer with Surface Indentations

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

    Dr Shahid Mughal

  6. Destabilisation of Stationary and Travelling Crossflow Disturbances Due to Steps over a Swept Wing

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

    Dr Shahid Mughal

  7. Control of boundary layer instabilities with plasma actuation

    Article • Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering, April 2019, SAGE Publications

    Dr Shahid Mughal

  8. Effect of Small Surface Deformations on the Stability of Tollmien–Schlichting Disturbances

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

    Alejandro Martinez-Cava, Dr Shahid Mughal, Christian Thomas

  9. The process of how smooth laminar air flows become turbulent while flowing over a rough surface

    Article • Physics of Fluids, April 2018, American Institute of Physics

    Dr Shahid Mughal

  10. Stability of an Infinite Swept Wing Boundary Layer with Surface Waviness

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

    Dr Shahid Mughal, Alejandro Martinez-Cava

  11. The Interaction of a Swept-Wing Boundary Layer with Surface Excrescences

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

    Professor Jonathan F Morrison, Dr Shahid Mughal

  12. Uncertainty Quantification Based Receptivity Modelling of Crossflow Instabilities Induced by Distributed Surface Roughness in Swept Wing Boundary Layers

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

    Dr Shahid Mughal

  13. Modeling of Natural Transition in Properly Three-Dimensional Flows

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

    Dr Shahid Mughal

  14. Stability Analysis of Complex Wing Geometries: Parabolised Stability Equations in Generalised Non-Orthogonal Coordinates.

    Article • June 2006, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Shahid Mughal