All Stories

  1. Aerodynamic Shape Optimisation Using a Machine Learning-Augmented Turbulence Model

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

    Prof Ning Qin

  2. A Priori Sensor Placement Strategy for Turbulent Mean Flow Reconstruction Using Parametric Model Perturbations

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

    Prof Ning Qin

  3. Cross-Field Structured Adaptive Mesh Using Medial Axis Flow Feature Extraction

    Article • AIAA Journal, October 2023, American Institute of Aeronautics and Astronautics (AIAA)

    Prof Ning Qin

  4. An Open-Source Adjoint-based Field Inversion Tool for Data-driven RANS modelling

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

    Prof Ning Qin

  5. Turbulent Mean Flow Reconstruction Based on Sparse Multi-sensor Data and Adjoint-based Field Inversion

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

    Prof Ning Qin

  6. Hybrid Mesh Deformation for Aerodynamic-Structural Coupled Adjoint Optimization

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

    Prof Ning Qin

  7. Vortex-Generating Shock Control Bumps for Robust Drag Reduction at Transonic Speeds

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

    Prof Ning Qin

  8. Balancing Laminar Extension and Wave Drag for Transonic Swept Wings

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

    Prof Ning Qin

  9. Influence of Spanwise Load Distribution on Blended-Wing–Body Performance at Transonic Speed

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

    Prof Ning Qin, Yonghong Li

  10. Quantification of Airfoil Aerodynamic Uncertainty due to Pressure-Sensitive Paint Thickness

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

    Prof Ning Qin

  11. Shock Control of a Low-Sweep Transonic Laminar Flow Wing

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

    Prof Ning Qin, feng deng, Yonghong Li

  12. Using the Reynolds Stress Model to Predict Shock-Induced Separation on Transport Aircraft

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

    Prof Ning Qin, Razvan Apetrei

  13. Nonconsistent Mesh Movement and Sensitivity Calculation on Adjoint Aerodynamic Optimization

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

    Benjamin Hinchliffe, Prof Ning Qin

  14. Spike Effects on Drag Reduction for Hypersonic Lifting Body

    Article • Journal of Spacecraft and Rockets, November 2017, American Institute of Aeronautics and Astronautics (AIAA)

    Prof Ning Qin, Feng Xie

  15. Robustness of Natural Laminar Flow Airfoil Drag Optimization to Transition Amplification Factor

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

    Prof Ning Qin

  16. Efficient Method to Eliminate Mesh Sensitivity in Adjoint-Based Optimization

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

    Benjamin Hinchliffe, Prof Ning Qin

  17. Combined Hessian and Adjoint Error-Based Anisotropic Mesh Adaptation for Turbomachinery Flows

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

    Prof Ning Qin

  18. Effect of Non-Consistent Mesh Movements and Sensitivities on a Discrete Adjoint Based Aerodynamic Optimization

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

    Prof Ning Qin

  19. Local class shape transformation parameterization (l-CST) for airfoils

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

    Prof Ning Qin

  20. Using Surface Sensitivity from Mesh Adjoint for Transonic Wing Drag Reduction

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

    Prof Ning Qin, Benjamin Hinchliffe

  21. Using A Fast and Explicit Mesh Movement Method To Efficiently Compute Mesh Sensitivity

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

    Prof Ning Qin, Benjamin Hinchliffe

  22. Using surface sensitivity from mesh adjoint solution for transonic wing drag reduction

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

    Prof Ning Qin, Benjamin Hinchliffe

  23. Deformable Overset Grid

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

    Prof Ning Qin, Shuanghou Deng

  24. Novel Method to Calculate Vibrational Thermal Conduction in Hypersonic Nonequilibrium Flow

    Article • Journal of Thermophysics and Heat Transfer, January 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Prof Ning Qin

  25. Fluid Structure Interaction on a Flexible Micro Air Vehicle

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

    Prof Ning Qin

  26. Using Mesh Adjoint for Shock Bump Deployment and Optimisation on Transonic Wings

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

    Prof Ning Qin

  27. Geometric Representation of Flow Features Using the Medial Axis for Mesh Generation

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

    Prof Ning Qin

  28. Hybrid RANS/LES for active flow control

    Article • Aircraft Engineering and Aerospace Technology, April 2014, Emerald

    Prof Ning Qin

  29. Modelling roughness effects for transitional low Reynolds number aerofoil flows

    Article • Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering, April 2014, SAGE Publications

    Prof Ning Qin