All Stories

  1. Coupling study of supersonic turbine stage and two-dimensional hydrogen/air rotating detonation combustor
  2. Research on performance predictions using single-hole film cooling based on PointNet
  3. Reconstruction of turbine blade surface temperature based on data fusion
  4. Dynamics study of shock wave intersection under high-frequency sine oscillation incoming flow
  5. Large eddy simulation study of rotating detonation supersonic turbine nozzle generated by method of characteristics under oscillating incoming flow
  6. Large eddy simulation study on trailing edge cutback cooling with a whisker lip
  7. Numerical Investigation of a Turbine Stator with Nonaxisymmetric Endwall Profiling
  8. Deep learning method for fast prediction of film cooling performance
  9. Numerical Prediction of 45° Angled Ribs Effects on U-shaped Channels Heat Transfer and Flow under Multi Conditions
  10. Improvement of film cooling performance by trenched holes on turbine leading-edge models
  11. Stability analysis of asymmetric wakes
  12. Influences of trailing boundary layer velocity profiles on wake vortex formation in a high-subsonic-turbine cascade
  13. Investigation of 3D Blade Design on Flow Field and Performance of a Low Pressure Turbine Stage
  14. Application and Design of Multi-Impingement Cooling Channel in Turbine Blade Trail Edge
  15. Investigation on Pitch-Wise Non-Uniform and Inflecting Inlet Flow of Low-Speed Plane Cascade
  16. Aerodynamic and Heat Transfer Optimization of One Stage Air-Cooled Turbine
  17. Full Three-Dimensional Optimization Platform of Turbine Blades Considering the Film Cooling