All Stories

  1. Ice Shape Convergence in Multi-Step Ice Accretion Simulations over Straight Wings
  2. Monnalisa: Modelling Nonlinear Aerodynamics of Lifting Surfaces
  3. Multi-fidelity assessment of the aerodynamic performances of unconventional aircraft tail configurations
  4. Poly-dispersed Eulerian-Lagrangian particle tracking for in-flight icing applications
  5. How do Uncertain Flow Parameters Affect the Shock Pattern in Nonequilibrium Gas Flows Around Blunt Bodies?
  6. Optimization of a multi-layered heater for an electro-thermal ice protection system for a composite wing
  7. Numerical Simulations of a Horizontal Axis Wind Turbine in Icing Conditions With and Without Electro-Thermal Ice Protection System
  8. Assessment of the PoliMIce toolkit from the 1st AIAA Ice Prediction Workshop
  9. Simulation and Sensitivity Analysis of a Wing-Tip Mounted Propeller Configuration from the Workshop for Integrated Propeller Prediction (WIPP)
  10. Towards Real-Time In-Flight Ice Detection Systems via Computational Aeroacoustics and Machine Learning
  11. Oblique waves in steady supersonic flows of Bethe–Zel’dovich–Thompson fluids
  12. Non-ideal oblique shock waves
  13. Influence of a recessed step at the throat section of a supersonic nozzle
  14. Local Solution to the Unsteady Stefan Problem for In-Flight Ice Accretion Modeling
  15. Blockage and Three-Dimensional Effects in Wind-Tunnel Testing of Ice Accretion over Wings
  16. An Adaptive Conservative ALE Approach to Deal with Large Boundary Displacements in Three-Dimensional Inviscid Simulations
  17. Multifidelity Physics-Based Method for Robust Optimization Applied to a Hovering Rotor Airfoil
  18. Evidence of complex flow structures in a converging-diverging nozzle caused by a recessed step at the nozzle throat
  19. Extension of the SU2 open source CFD code to the simulation of turbulent flows of fuids modelled with complex thermophysical laws
  20. A model for in-flight ice accretion based on the exact solution of the unsteady Stefan problem
  21. Drag minimization of an isolated airfoil in transonic inviscid flow by means of genetic algorithms
  22. Robust aerodynamic optimization of morphing airfoils for helicopter rotor blades