All Stories

  1. Refined entropy analysis in turbine cascade: A novel loss decomposition method for flow with large separation
  2. A comprehensive study on the impact of turbomachinery synergy on the thermodynamic performance of supercritical carbon dioxide reheated recompression cycle
  3. Heat transfer enhancement mechanism of supercritical pressure fluids in circular pipes under transverse vibration
  4. Nonlinear uncertain impact of geometric deviations on aerodynamic performance with different design parameters in transonic high-pressure turbine
  5. Layout and Rotation Effect on Aerodynamic Performance of Multi-Rotor Ducted Propellers
  6. Aerothermal performance of turbine during flight cycle based on fluid-thermal-structure multidisciplinary coupling method
  7. Impact of multiscale flow structures on mixing and losses in turbine blade tip region
  8. Numerical investigation on aerodynamic characteristics of equivalent distributed ducted propellers
  9. Knowledge enhanced modeling of low-pressure turbine profile loss by combining physical-based and data-driven methods
  10. Multi-stage radial-outflow supercritical carbon dioxide turbines: Preliminary design and optimization with insights into 3D design and structural considerations
  11. Augmentation of predictive turbulence modeling applied to low pressure turbines using adaptive field inversion
  12. A Multi-Dimensional Life Cycle Assessment Framework for Integrated Propulsion-Energy Management in Hypersonic Vehicles
  13. Research on multi-disciplinary coupling mechanism between internal flow heat transfer and solid deformation in turbine
  14. A novel dual-stage failure criterion based on forming limit curve for uncured GLARE
  15. Development of a tip leakage loss model for high-pressure turbines with squealer tips based on physics-driven and data-driven methods
  16. Insights into thermodynamic performance of a hypersonic precooled air-breathing engine with a complicated multi-branch closed cycle
  17. Failure analysis and formability improvement of GLARE laminates in warm active hydroforming technology: Experimental and numerical approach
  18. Application of artificial intelligence in turbomachinery aerodynamics: progresses and challenges
  19. Thermodynamic performance study of simplified precooled engine cycle with coupling power output
  20. Experimental and numerical investigation on rotating stall flow pattern in a counter-rotating axial compressor
  21. Development of helium turbine loss model based on knowledge transfer with neural network and its application on aerodynamic design
  22. Nonlinear uncertainty impact of geometric variations on aerodynamic performance of low-pressure turbine blades with ultra-high loading under extreme operational conditions
  23. A comprehensive preliminary design methodology and an optimization workflow for single-stage radial-outflow turbines and application for 10 MW sCO2 turbines
  24. A novel active hydroforming & curing process to manufacture GLARE laminates: Numerical and experimental investigations
  25. Uncertainty quantification of geometric variations in transonic high-pressure turbine with different trailing edge and throat area distribution
  26. An evaluation model for wall heat transfer effects on micro centrifugal compressors and its application in aerodynamic design
  27. Statistical investigations of profile error impact on flow and performance of a low-pressure turbine cascade
  28. Experimental insights into thermal performance of a microtube precooler with drastic coolant properties variation and precooling impacts on turbojet engine operation
  29. A Review of the Complex Flow and Heat Transfer Characteristics in Microchannels
  30. Refined flow organization in squealer tip gap and its impact on turbine aerodynamic performance
  31. Uncertainty analysis of measured geometric variations in turbine blades and impact on aerodynamic performance
  32. Large eddy simulations of periodic wake effects on boundary-layer transition of low-pressure turbine cascades
  33. Performance Assessment of the Advanced Precooled Airbreathing Engine with Complicated Multi-Branch Closed Brayton Cycle
  34. Impact of complex flow structures on the turbine blade tip region mixing
  35. Investigation into a comprehensive forming limit curve considering multi-parameters effects for semi-cured FMLs through uniform pressure loading test
  36. Aerodynamic design considerations for supercritical CO2 centrifu...
  37. Effect of loading level and axial distribution on uncertainty performance of turbine blade with geometric variations
  38. Knowledge-based turbomachinery design system via a deep neural network and multi-output Gaussian process
  39. A study of real-gas effect on SCO<sub>2</sub> compressor performance using similitude method
  40. Thermal-hydraulic characteristics of a PCHE with zigzag microchannel for hypersonic precooled aero-engines: an experimental study
  41. Experimental Hydraulic Performance Study of a Primary Surface Recuperator With Cross-Wavy Microchannels for Portable Microturbines
  42. Large Eddy Simulation on the Turbulent Heat Transfer of Supercritical Fluid
  43. Mixing Mechanism of Multi-Scale Flow in Tip Region of Turbine Rotor
  44. Calibration and validation of fatigue lifetime model in complex structures based on multi-level data
  45. A Reliable Update of the Ainley and Mathieson Profile and Secondary Correlations
  46. Large-Eddy Simulation on the Aerodynamic and Thermal Characteristics in a Micropipe of the Hypersonic Engine Precooler
  47. An investigation on AerofoilShaped Blade Profiles for Centrifugal Turbines
  48. A novel simplified precooled airbreathing engine cycle: Thermodynamic performance and control law
  49. Thermal performance of a microchannel primary surface recuperator for portable microturbine generators: Design and experimental study
  50. A refined design method for precoolers with consideration of multi-parameter variations based on low-dimensional analysis
  51. Verification at Mach 4 heat conditions of an annular microtube-typed precooler for hypersonic precooled engines
  52. Statistical and Computational Evaluation of Empirical Axial Turbine Correlations in Design of Centrifugal Turbines
  53. A unified performance conversion method for similar compressors working with different gases based on polytropic analysis and deep-learning improvement
  54. Effects of Squealer Geometry of Turbine Blade Tip on the Tip-Leakage Flow and Loss
  55. Influence of Supercritical Carbon Dioxide Condensation on Flow and Performance
  56. Numerical investigation into the structural characteristics of a hydrogen dual-swirl combustor with slight temperature rise combustion
  57. Micromanufacturing technologies of compact heat exchangers for hypersonic precooled airbreathing propulsion: A review
  58. A hybrid performance prediction method for centrifugal compressors based on single-zone and two-zone models
  59. Experimental study and performance analysis of high-performance micro-channel heat exchanger for hypersonic precooled aero-engine
  60. Design optimization, construction and testing of 2 K Joule-Thomson heat exchanger for a superfluid helium cryogenic system
  61. A one-dimensional design methodology for supercritical carbon dioxide Brayton cycles: Integration of cycle conceptual design and components preliminary design
  62. Statistical and Computational Evaluation of Axial Loss Correlations Applied to Centrifugal Turbines
  63. An experimental method for squealer tip flow field considering relative casing motion
  64. The Development and Applications of a Loading Distribution Based Tip Leakage Loss Model for Unshrouded Gas Turbines
  65. Effects of flow structure on heat transfer of squealer tip in a turbine rotor blade
  66. Energy dissipation analysis based on velocity gradient tensor decomposition
  67. Effects of heat transfer on separated boundary layer behavior under adverse pressure gradients
  68. Numerical Investigation on Metrological Fidelity of a Shielded Thermocouple Probe and the Effects of Geometrical Parameters
  69. A study on the similarity method for helium compressors
  70. Thermal performance analysis and operation of the spoke cavity cryomodules for C-ADS Injector-I
  71. Design and thermal performance of spoke cavity prototype cryomodule of the Chinese Accelerator Driven Sub-critical system Injector-I
  72. Uncertainty analysis of impact of geometric variations on turbine blade performance
  73. Large Eddy Simulations of Separated Boundary Layer With Pressure Gradient and Heat Transfer
  74. Aerodynamic design method of micro-scale radial turbines considering the effect of wall heat transfer
  75. Overall performance design of paralleled heat release and compression system for hypersonic aeroengine
  76. Numerical modeling of steady state errors for shielded thermocouples based on conjugate heat transfer analysis
  77. A new similarity method for turbomachinery with different working media
  78. Axial Turbine Aerodynamics for Aero-engines
  79. Fundamental Concepts
  80. Flow Control Technologies
  81. Multidisciplinary Coupling Analysis and Design
  82. Aerodynamic Design Technologies for Turbines
  83. Dominant flow structure in the squealer tip gap and its impact on turbine aerodynamic performance
  84. Experimental study on the flow and heat transfer mechanism of the pre-cooler in the hypersonic aeroengine
  85. Experimental study on compact heat exchanger for hypersonic aero-engine
  86. NUMERICAL STUDY OF POROUS BLUNT NOSECONE TRANSPIRATION COOLING UNDER SUPERSONIC INCOMING FLOW
  87. Shroud leakage flow models and a multi-dimensional coupling CFD (computational fluid dynamics) method for shrouded turbines
  88. Aerodynamic Design and Numerical Analysis of Supersonic Turbine for Turbo Pump
  89. Aerodynamic impact of hub and shroud leakage flow on an axial turbine stage
  90. Large Eddy Simulations of Separated Shear Layer Behaviors in a High-Lift LP Turbine
  91. Experimental investigation on the effects of wake passing frequency on boundary layer transition in high-lift low-pressure turbines
  92. Effects of freestream turbulence on separated boundary layer in a low-Re high-lift LP turbine blade
  93. Investigations of Heat Transfer Enhancement in a Channel with Staggered Porous Ribs by the Preconditioned Density-Based Algorithm
  94. Aerothermal Analysis of a Turbine With Rim Seal Cavity
  95. Effect of surface roughness on the aerodynamic performance of turbine blade cascade
  96. Influence of turbulence model parameter settings on conjugate heat transfer simulation
  97. A novel multi-fidelity coupled simulation method for flow systems
  98. Conjugate heat transfer investigations of turbine vane based on transition models
  99. Conjugate heat transfer investigation of cooled turbine using the preconditioned density-based algorithm
  100. Robust and Quality Boundary Constrained Tetrahedral Mesh Generation
  101. Improvement of a Turbulence Model for Conjugate Heat Transfer Simulation
  102. Numerical Investigation of Laminar-Plate Transpiration Cooling by the Preconditioned Density-Based Algorithm
  103. Effects of Periodic Wakes and Freestream Turbulence on Coherent Structures in Low-Pressure Turbine Boundary Layer
  104. Leading-edge redesign of a turbomachinery blade and its effect on aerodynamic performance
  105. Unsteady Flows in Turbines
  106. High altitude low Reynolds number effect on the matching performance of a turbofan engine
  107. Investigation of a Confined Laminar Impinging Jet on a Plate with a Porous Layer Using the Preconditioned Density-Based Algorithm
  108. Control of secondary flow loss in turbine cascade by streamwise vortex
  109. Investigation of metallic foam in the application of turbine cooling
  110. Preconditioned Density-Based Algorithm for Conjugate Porous/Fluid/Solid Domains
  111. Upstream wake–secondary flow interactions in the endwall region of high-loaded turbines
  112. Impact of stagger angle nonuniformity on turbine aerodynamic performance
  113. Boundary layer separation control on a highly-loaded, low-solidity compressor cascade
  114. Analysis of Flow Mechanism in 2-D Compressor Cascade With Splitter
  115. Flow Analysis on a Single-Stage Axial Compressor With a Splitter Rotor
  116. Hierarchical structures in a turbulent pipe flow
  117. Extended self-similarity and hierarchical structure in turbulence