All Stories

  1. Uncertainty quantification of geometric variations in transonic high-pressure turbine with different trailing edge and throat area distribution
  2. An evaluation model for wall heat transfer effects on micro centrifugal compressors and its application in aerodynamic design
  3. Statistical investigations of profile error impact on flow and performance of a low-pressure turbine cascade
  4. Experimental insights into thermal performance of a microtube precooler with drastic coolant properties variation and precooling impacts on turbojet engine operation
  5. A Review of the Complex Flow and Heat Transfer Characteristics in Microchannels
  6. Refined flow organization in squealer tip gap and its impact on turbine aerodynamic performance
  7. Uncertainty analysis of measured geometric variations in turbine blades and impact on aerodynamic performance
  8. Large eddy simulations of periodic wake effects on boundary-layer transition of low-pressure turbine cascades
  9. Performance Assessment of the Advanced Precooled Airbreathing Engine with Complicated Multi-Branch Closed Brayton Cycle
  10. Impact of complex flow structures on the turbine blade tip region mixing
  11. Investigation into a comprehensive forming limit curve considering multi-parameters effects for semi-cured FMLs through uniform pressure loading test
  12. Aerodynamic design considerations for supercritical CO2 centrifu...
  13. Effect of loading level and axial distribution on uncertainty performance of turbine blade with geometric variations
  14. Knowledge-based turbomachinery design system via a deep neural network and multi-output Gaussian process
  15. A study of real-gas effect on SCO<sub>2</sub> compressor performance using similitude method
  16. Thermal-hydraulic characteristics of a PCHE with zigzag microchannel for hypersonic precooled aero-engines: an experimental study
  17. Experimental Hydraulic Performance Study of a Primary Surface Recuperator With Cross-Wavy Microchannels for Portable Microturbines
  18. Large Eddy Simulation on the Turbulent Heat Transfer of Supercritical Fluid
  19. Mixing Mechanism of Multi-Scale Flow in Tip Region of Turbine Rotor
  20. Calibration and validation of fatigue lifetime model in complex structures based on multi-level data
  21. A Reliable Update of the Ainley and Mathieson Profile and Secondary Correlations
  22. Large-Eddy Simulation on the Aerodynamic and Thermal Characteristics in a Micropipe of the Hypersonic Engine Precooler
  23. An investigation on AerofoilShaped Blade Profiles for Centrifugal Turbines
  24. A novel simplified precooled airbreathing engine cycle: Thermodynamic performance and control law
  25. Thermal performance of a microchannel primary surface recuperator for portable microturbine generators: Design and experimental study
  26. A refined design method for precoolers with consideration of multi-parameter variations based on low-dimensional analysis
  27. Verification at Mach 4 heat conditions of an annular microtube-typed precooler for hypersonic precooled engines
  28. Statistical and Computational Evaluation of Empirical Axial Turbine Correlations in Design of Centrifugal Turbines
  29. A unified performance conversion method for similar compressors working with different gases based on polytropic analysis and deep-learning improvement
  30. Effects of Squealer Geometry of Turbine Blade Tip on the Tip-Leakage Flow and Loss
  31. Influence of Supercritical Carbon Dioxide Condensation on Flow and Performance
  32. Numerical investigation into the structural characteristics of a hydrogen dual-swirl combustor with slight temperature rise combustion
  33. Micromanufacturing technologies of compact heat exchangers for hypersonic precooled airbreathing propulsion: A review
  34. A hybrid performance prediction method for centrifugal compressors based on single-zone and two-zone models
  35. Experimental study and performance analysis of high-performance micro-channel heat exchanger for hypersonic precooled aero-engine
  36. Design optimization, construction and testing of 2 K Joule-Thomson heat exchanger for a superfluid helium cryogenic system
  37. A one-dimensional design methodology for supercritical carbon dioxide Brayton cycles: Integration of cycle conceptual design and components preliminary design
  38. Statistical and Computational Evaluation of Axial Loss Correlations Applied to Centrifugal Turbines
  39. An experimental method for squealer tip flow field considering relative casing motion
  40. The Development and Applications of a Loading Distribution Based Tip Leakage Loss Model for Unshrouded Gas Turbines
  41. Effects of flow structure on heat transfer of squealer tip in a turbine rotor blade
  42. Energy dissipation analysis based on velocity gradient tensor decomposition
  43. Effects of heat transfer on separated boundary layer behavior under adverse pressure gradients
  44. Numerical Investigation on Metrological Fidelity of a Shielded Thermocouple Probe and the Effects of Geometrical Parameters
  45. A study on the similarity method for helium compressors
  46. Thermal performance analysis and operation of the spoke cavity cryomodules for C-ADS Injector-I
  47. Design and thermal performance of spoke cavity prototype cryomodule of the Chinese Accelerator Driven Sub-critical system Injector-I
  48. Uncertainty analysis of impact of geometric variations on turbine blade performance
  49. Large Eddy Simulations of Separated Boundary Layer With Pressure Gradient and Heat Transfer
  50. Aerodynamic design method of micro-scale radial turbines considering the effect of wall heat transfer
  51. Overall performance design of paralleled heat release and compression system for hypersonic aeroengine
  52. Numerical modeling of steady state errors for shielded thermocouples based on conjugate heat transfer analysis
  53. A new similarity method for turbomachinery with different working media
  54. Axial Turbine Aerodynamics for Aero-engines
  55. Fundamental Concepts
  56. Flow Control Technologies
  57. Multidisciplinary Coupling Analysis and Design
  58. Aerodynamic Design Technologies for Turbines
  59. Dominant flow structure in the squealer tip gap and its impact on turbine aerodynamic performance
  60. Experimental study on the flow and heat transfer mechanism of the pre-cooler in the hypersonic aeroengine
  61. Experimental study on compact heat exchanger for hypersonic aero-engine
  62. NUMERICAL STUDY OF POROUS BLUNT NOSECONE TRANSPIRATION COOLING UNDER SUPERSONIC INCOMING FLOW
  63. Shroud leakage flow models and a multi-dimensional coupling CFD (computational fluid dynamics) method for shrouded turbines
  64. Aerodynamic Design and Numerical Analysis of Supersonic Turbine for Turbo Pump
  65. Aerodynamic impact of hub and shroud leakage flow on an axial turbine stage
  66. Large Eddy Simulations of Separated Shear Layer Behaviors in a High-Lift LP Turbine
  67. Experimental investigation on the effects of wake passing frequency on boundary layer transition in high-lift low-pressure turbines
  68. Effects of freestream turbulence on separated boundary layer in a low-Re high-lift LP turbine blade
  69. Investigations of Heat Transfer Enhancement in a Channel with Staggered Porous Ribs by the Preconditioned Density-Based Algorithm
  70. Aerothermal Analysis of a Turbine With Rim Seal Cavity
  71. Effect of surface roughness on the aerodynamic performance of turbine blade cascade
  72. Influence of turbulence model parameter settings on conjugate heat transfer simulation
  73. A novel multi-fidelity coupled simulation method for flow systems
  74. Conjugate heat transfer investigations of turbine vane based on transition models
  75. Conjugate heat transfer investigation of cooled turbine using the preconditioned density-based algorithm
  76. Robust and Quality Boundary Constrained Tetrahedral Mesh Generation
  77. Improvement of a Turbulence Model for Conjugate Heat Transfer Simulation
  78. Numerical Investigation of Laminar-Plate Transpiration Cooling by the Preconditioned Density-Based Algorithm
  79. Effects of Periodic Wakes and Freestream Turbulence on Coherent Structures in Low-Pressure Turbine Boundary Layer
  80. Leading-edge redesign of a turbomachinery blade and its effect on aerodynamic performance
  81. Unsteady Flows in Turbines
  82. High altitude low Reynolds number effect on the matching performance of a turbofan engine
  83. Investigation of a Confined Laminar Impinging Jet on a Plate with a Porous Layer Using the Preconditioned Density-Based Algorithm
  84. Control of secondary flow loss in turbine cascade by streamwise vortex
  85. Investigation of metallic foam in the application of turbine cooling
  86. Preconditioned Density-Based Algorithm for Conjugate Porous/Fluid/Solid Domains
  87. Impact of stagger angle nonuniformity on turbine aerodynamic performance
  88. Boundary layer separation control on a highly-loaded, low-solidity compressor cascade
  89. Analysis of Flow Mechanism in 2-D Compressor Cascade With Splitter
  90. Flow Analysis on a Single-Stage Axial Compressor With a Splitter Rotor
  91. Hierarchical structures in a turbulent pipe flow
  92. Extended self-similarity and hierarchical structure in turbulence