All Stories

  1. Direct solution of an analytical model to investigate duct acoustic treatments at low and high frequencies
  2. Application of a Novel Pseudo-Spectral Time-Marching Method to Turbomachinery
  3. Conceptual Analysis on the Impact of Acoustic Liners in Fan Flutter
  4. Mach number influence on low-pressure turbine flutter
  5. Time-Inclined Method for High-Fidelity Rotor/Stator Simulations
  6. Impact of three-dimensional turbulence modelling on rotor/stator interaction broadband noise
  7. Effective Clearance and Differential Gapping Impact on Seal Flutter Modeling and Validation
  8. Turbine Broadband Noise Predictions Using Linearised Frequency Domain Navier-Stokes Solvers
  9. Numerical validation of an analytical seal flutter model
  10. Prediction of fan acoustic blockage on fan/outlet guide vane broadband interaction noise using frequency domain linearised Navier–Stokes solvers
  11. Higher Order Conceptual Model for Labyrinth Seal Flutter
  12. Nonlinear Stability Analysis of a Generic Fan With Distorted Inflow Using Passage-Spectral Method
  13. Numerical and Experimental Investigation of the Reynolds Number and Reduced Frequency Effects on Low-Pressure Turbine Airfoils
  14. Efficient Passage-Spectral Method For Unsteady Flows Under Stall Conditions
  15. Conceptual Flutter Analysis of Stepped Labyrinth Seals
  16. Prediction of Reynolds Number Effects on Low-Pressure Turbines Using a High-Order ILES Method
  17. Tip-Shroud Labyrinth Seal Effect on the Flutter Stability of Turbine Rotor Blades
  18. Accelerating advancing layer viscous mesh generation for 3D complex configurations
  19. Conceptual Flutter Analysis of Stepped Labyrinth Seals
  20. Efficient Passage-Spectral Method for Unsteady Flows Under Stall Conditions
  21. Prediction of Reynolds Number Effects on Low-Pressure Turbines Using a High-Order ILES Method
  22. Tip-Shroud Labyrinth Seal Effect on the Flutter Stability of Turbine Rotor Blades
  23. Implicit Large Eddy Simulation of Low Pressure Turbine Airfoils Using a High Order Navier-Stokes Solver
  24. Flutter Generation and Control Using Mistuning in a Turbine Rotating Rig
  25. Numerical study of uneven wall-heating effect for a one side rib-roughened cooling channel subject to rotation
  26. On the transient behaviour of a laminar rotor–stator cavity
  27. Conceptual Flutter Analysis of Labyrinth Seals Using Analytical Models—Part I: Theoretical Support
  28. Conceptual Flutter Analysis of Labyrinth Seals Using Analytical Models—Part II: Physical Interpretation
  29. Design of mistuning patterns to control the vibration amplitude of unstable rotor blades
  30. An efficient steady state coupled fluid-solid heat transfer method for turbomachinery applications
  31. PHYSICAL APPROACH OF COMPUTATIONAL FLUID DYNAMICS FOR UNDERGRADUATE ENGINEERING STUDENTS
  32. Robust Method to Solve Meanline Equations for Choked Flows
  33. Comparison between aerodynamic designs obtained by human driven and automatic procedures
  34. Effect of Uneven Wall Heating Conditions Under Different Buoyancy Numbers for a One Side Rib-Roughened Rotating Channel
  35. Accurate Method to Reproduce Throughflow Results With a Meanline Solver
  36. Comparing Human Driven and Automatic Blade Row Aerodynamic Designs
  37. Effect of Uneven Wall Heating Conditions Under Different Buoyancy Numbers for a One Side Rib-Roughened Rotating Channel
  38. Execution of a parallel edge-based Navier–Stokes solver on commodity graphics processor units
  39. Accelerating advancing layer viscous mesh generation for 3D complex configurations
  40. Quantification of the Influence of Unsteady Aerodynamic Loading on the Damping Characteristics of Airfoils Oscillating at Low Reduced Frequency—Part II: Numerical Verification
  41. Quantification of the Influence of Unsteady Aerodynamic Loading on the Damping Characteristics of Airfoils Oscillating at Low-Reduced Frequency—Part I: Theoretical Support
  42. Experimental and Numerical Study of Heat Transfer Performance for an Engine Representative Two-Pass Rotating Internal Cooling Channel
  43. Flutter Generation and Control Using Mistuning in a Turbine Rotating Rig
  44. The Low Reduced Frequency Limit of Vibrating Airfoils: Part IIIA — Theoretical Quantification and Influence of Unsteady Loading
  45. The Low Reduced Frequency Limit of Vibrating Airfoils: Part IIIB — Numerical Quantification and Influence of Unsteady Loading
  46. Two-Dimensional Airfoil Shape Optimization Using Highly Differentiable Splines and Evolution Strategies
  47. Turbomachinery Aerodynamic Damping at Low vibration frequency
  48. A Novel Mixing Plane Method Using Nonreflecting Boundary Conditions for Multirow Analysis in Turbomachines
  49. An Implicit Harmonic Balance Method in Graphics Processing Units for Oscillating Blades
  50. The Low Reduced Frequency Limit of Vibrating Airfoils—Part I: Theoretical Analysis
  51. The Low Reduced Frequency Limit of Vibrating Airfoils—Part II: Numerical Experiments
  52. A Loosely Coupled Fluid/Solid Heat Transfer Method for Disc Cavities Including Mixing Planes and a Combination of 2D and 3D Cavities
  53. An Implicit Harmonic Balance Method in Graphics Processing Units for Vibrating Blades
  54. The Low Reduced Frequency Limit of Vibrating Airfoils: Part I — Theoretical Analysis
  55. The Low Reduced Frequency Limit of Vibrating Airfoils: Part II — Numerical Experiments
  56. A Novel Mixing Plane Method Using Non-Reflecting Boundary Conditions for Multi-Row Analysis in Turbomachines
  57. Flutter Amplitude Saturation by Nonlinear Friction Forces: Reduced Model Verification
  58. A Study on the Effects of Geometric Non Linearities on the Un-Running Transformation of Compressor Blades
  59. Experimental and Numerical Assessment of the Aeroelastic Stability of Blade Pair Packages
  60. Flutter Amplitude Saturation by Nonlinear Friction Forces: Reduced Model Validation
  61. Flutter or turbines with multiple unstable modes.
  62. Validation of a simple model to study the response of turbine rotors with imperfections.
  63. Asymptotic description of damping mistuning effects on the forced response of turbomachinery bladed disks
  64. Physics of Vibrating Airfoils at Low Reduced Frequency
  65. Analysis and Improvement of a Loosely Coupled Fluid-Solid Heat Transfer Method
  66. Application of a Fast Loosely Coupled Fluid/Solid Heat Transfer Method to the Transient Analysis of Low-Pressure-Turbine Disk Cavities
  67. Conceptual Analysis of the Non-Linear Forced Response of Aerodynamically Unstable Bladed-Discs
  68. Flutter Amplitude Saturation by Nonlinear Friction Forces: An Asymptotic Approach
  69. Interaction of Rim Seal and Main Annulus Flow in a Low-Speed Turbine Rig
  70. Using genetic algorithms to improve the thermodynamic efficiency of gas turbines designed by traditional methods
  71. Prediction protocol for neurological outcome for survivors of out-of-hospital cardiac arrest treated with targeted temperature management
  72. Effect of the Structural Coupling on the Flutter Onset of a Sector of Low-Pressure Turbine Vanes
  73. Development of an Edge-Based Harmonic Balance Method for Turbomachinery Flows
  74. Forced Response of Bladed Disks With Damping Mistuning
  75. Implementation of an Edge-Based Navier-Stokes Solver for Unstructured Grids in Graphics Processing Units
  76. Non-Linear Dynamics of Multi-Mode Unstable Bladed-Disks: Part I—Description of a Canonical Model and Phenomenological Results
  77. Numerical Assessment of the Noise Signature Sidewall Contamination of a Linear Cascade With Moving Bars
  78. Turbomachinery Thermal Analysis Using Coupled Two- and Three Dimensional Models and Reduced Order Fluid Models
  79. Validation of a Coupled Fluid/Solid Heat Transfer Method
  80. Efficient Edge-Based Rotor/Stator Interaction Method
  81. Optimisation of axially segmented liners for aeroengine broadband noise
  82. Effect of the Structural Coupling on the Flutter Onset of a Sector of Low-Pressure Turbine Vanes
  83. Optimizing the Number of Airfoils in Turbine Design Using Genetic Algorithms
  84. Prediction of Separation-Induced Transition Using a Correlation-Based Transition Model
  85. Quantitative Validation of the Asymptotic Mistuning Model Using a High Fidelity Bladed Disk Model
  86. Rapid meshing of turbomachinery rows using semi-unstructured multi-block conformal grids
  87. A Conceptual Flutter Analysis of a Packet of Vanes Using a Mass-Spring Model
  88. A Hybrid Unstructured/Spectral Method for the Resolution of Navier-Stokes Equations
  89. Asymptotic Description of Maximum Mistuning Amplification of Bladed Disk Forced Response
  90. Validation of an Efficient Unstructured Time-Domain Rotor/Stator Interaction Method
  91. Asymptotic Description of Maximum Mistuning Amplification of Bladed Disk Forced Response
  92. Cavity Effects on the Design of Turbine Profiled End Walls
  93. Numerical Assessment of the Noise Signature Sidewall Contamination of a Linear Cascade With Moving Bars
  94. Profiled End Wall Design Using an Adjoint Navier–Stokes Solver
  95. Stability Increase of Aerodynamically Unstable Rotors Using Intentional Mistuning
  96. Verification of the Vibration Amplitude Prediction of Self-Excited LPT Rotor Blades Using a Fully Coupled Time-Domain Non-Linear Method and Experimental Data
  97. Aeroelastic Instability of Low-Pressure Rotor Blades
  98. A Conceptual Flutter Analysis of a Packet of Vanes Using a Mass-Spring Model
  99. Aeroelastic Stability of Welded-in-Pair Low Pressure Turbine Rotor Blades: A Comparative Study Using Linear Methods
  100. A Methodology for the Vibration Amplitude Prediction of Self-Excited Rotors Based on Dimensional Analysis
  101. Profiled End-Wall Design Using an Adjoint Navier-Stokes Solver
  102. Stability Increase of Aerodynamically Unstable Rotors Using Intentional Mistuning
  103. Effect of Sidewall Contamination on Linear Cascades With Moving Bars
  104. Parametric Design of Turbomachinery Airfoils Using Highly Differentiable Splines
  105. A Numerical Investigation on the Influence of Lateral Boundaries in Linear Vibrating Cascades
  106. A Numerical Investigation on the Influence of Lateral Boundaries in Linear Vibrating Cascades
  107. Semi-Unstructured Grid Methods for Turbomachinery Applications
  108. Application of Phase-Lagged Boundary Conditions to Rotor/Stator Interaction
  109. Surface Mesh Generation by Means of Steiner Triangulations
  110. Surface mesh generation by means of Steiner triangulations
  111. Influence of the Artificial Dissipation Model on the Propagation of Acoustic and Entropy Waves
  112. Quantitative Influence of the Steady Non-Reflecting Boundary Conditions on Blade-to-Blade Computations
  113. A Parametric Design Tool for Cascades of Airfoils
  114. Surface mesh generation by means of Steiner triangulations
  115. Fourier/Chebyshev methods for the incompressible Navier-Stokes equations in infinite domains
  116. Rapid Meshing of Turbomachinery Rows Using Semi-Unstructured Conformal Grids
  117. FLUTTER BOUNDARIES FOR PAIRS OF LOW PRESSURE TURBINE BLADES