All Stories

  1. An Open-Source Adjoint-based Field Inversion Tool for Data-driven RANS modelling
  2. Turbulent Mean Flow Reconstruction Based on Sparse Multi-sensor Data and Adjoint-based Field Inversion
  3. Hybrid Mesh Deformation for Aerodynamic-Structural Coupled Adjoint Optimization
  4. Vortex-Generating Shock Control Bumps for Robust Drag Reduction at Transonic Speeds
  5. Balancing Laminar Extension and Wave Drag for Transonic Swept Wings
  6. Influence of Spanwise Load Distribution on Blended-Wing–Body Performance at Transonic Speed
  7. Quantification of Airfoil Aerodynamic Uncertainty due to Pressure-Sensitive Paint Thickness
  8. Shock Control of a Low-Sweep Transonic Laminar Flow Wing
  9. Using the Reynolds Stress Model to Predict Shock-Induced Separation on Transport Aircraft
  10. Nonconsistent Mesh Movement and Sensitivity Calculation on Adjoint Aerodynamic Optimization
  11. Spike Effects on Drag Reduction for Hypersonic Lifting Body
  12. Robustness of Natural Laminar Flow Airfoil Drag Optimization to Transition Amplification Factor
  13. Efficient Method to Eliminate Mesh Sensitivity in Adjoint-Based Optimization
  14. Combined Hessian and Adjoint Error-Based Anisotropic Mesh Adaptation for Turbomachinery Flows
  15. Effect of Non-Consistent Mesh Movements and Sensitivities on a Discrete Adjoint Based Aerodynamic Optimization
  16. Local class shape transformation parameterization (l-CST) for airfoils
  17. Using Surface Sensitivity from Mesh Adjoint for Transonic Wing Drag Reduction
  18. Using A Fast and Explicit Mesh Movement Method To Efficiently Compute Mesh Sensitivity
  19. Using surface sensitivity from mesh adjoint solution for transonic wing drag reduction
  20. Deformable Overset Grid
  21. Novel Method to Calculate Vibrational Thermal Conduction in Hypersonic Nonequilibrium Flow
  22. Fluid Structure Interaction on a Flexible Micro Air Vehicle
  23. Using Mesh Adjoint for Shock Bump Deployment and Optimisation on Transonic Wings
  24. Geometric Representation of Flow Features Using the Medial Axis for Mesh Generation
  25. Hybrid RANS/LES for active flow control
  26. Modelling roughness effects for transitional low Reynolds number aerofoil flows