All Stories

  1. Nonparallel, Nonlocall Flow Stability Analysis Through a Physics-Informed Data-Driven Approach
  2. Influence of Park's Two-Temperature Model Control Temperature on the Flow Properties in Hypersonic Reentry Conditions
  3. Data-Driven Reduced-Order Modeling Techniques for Aeroelastic Analyses
  4. Transonic, High-Mach Number Wing Adjoint-Based Aerodynamic Shape Optimization
  5. Racing Car Wing Adjoint-Based Aerodynamic Shape Optimization
  6. A Comparison of LES Inlet Boundary Conditions for Supersonic Jet Flows
  7. Development of a Parallel High-Order CFD Solver with the Chapel Programming Language
  8. A Study on the Impact of Radiative Heat Transfer for Hypersonic Nonequilibrium Flows over a Cylinder
  9. An Analysis of Face Gradient Reconstruction Schemes for the Simulation of Aerospace Flows
  10. Study on the Resolution of Large-Eddy Simulations for Supersonic Jet Flows
  11. Numerical Simulation of Non-Equilibrium Hypersonic Flows for the Reentry Trajectory of a Reusable Satellite
  12. High-Fidelity Numerical Simulations of Supersonic Channel Flows with Isothermal Walls
  13. Investigation of Thermodynamic Non-Equilibrium in Hypersonic Flows Over the Mars Pathfinder Capsule
  14. Computational Static Aeroelastic Analyses in Transonic Flows
  15. Numerical Effects of Flux Calculation Schemes for Unstructured Grid Turbulent Flow Simulations
  16. Quantifying Uncertainty in Computational Fluid Dynamics Drag Computations on Unstructured Meshes
  17. DSMC Computations of SARA Reentry Capsule Exposed to Weakly Ionized Gas Flow
  18. An Evaluation of p-Multigrid and Local Mach Number Preconditioning with High Order FR/CPR Method
  19. Thermochemical Nonequilibrium Computations of a Brazilian Reentry Satellite
  20. Scalability Study of a Compressible LES solver
  21. Drag dispersion on cfd computations on unstrucrured grids
  22. High-Order Meshes for Flow Simulations with a Spectral Difference Method
  23. Investigation of Turbulence Properties in Wall-Bounded Flows with Pressure Gradients and Separation
  24. A Study of Efficiency of Implicit High-Order Spectral Difference Method Implementations
  25. Dynamic Mode Decomposition of High Reynolds Number Supersonic Jet Flows
  26. Influence of Different Subgrid Scale Models in LES of Supersonic Jet Flows
  27. Numerical Investigation of Channel Flows with Emphasis on Coherent Structures and Turbulence Anisotropy
  28. Implicit Spectral Difference Method Solutions of Compressible Flows Considering High-Order Meshes
  29. ONERA M6 simulation
  30. Inflow Turbulence Effects on Transition Prediction Using a Correlation-Based Transition Model
  31. Sound and Sources of Sound in a Model Problem with Wake Interaction
  32. Thermochemical Nonequilibrium Computations of a Brazilian Reentry Satellite
  33. Large Eddy Simulations of Supersonic Jet Flows for Aeroacoustic Applications
  34. Further Studies of Adverse Pressure Gradient Effects in Turbulent Channel Flows
  35. High-Order Compressible Flow Simulations with the Unstructured Spectral Difference Method
  36. Comparison of Viscous and Inviscid Unsteady Aerodynamic Loads for Aeroelastic Analyses
  37. A Numerical Study on Transitional Flows by Means of a Correlation-Based Transition Model
  38. Adverse Pressure Gradient Effects in the Turbulent Kinetic Energy Budget for Channel Flows
  39. A Comparative Study of Discontinuous High Order Methods for Compressible Flows
  40. An Assessment of Attached and Mildly Separated Flows in Adverse Pressure Gradient Regions