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Published/Copyright: December 1, 2025
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Published Online: 2025-12-01
Published in Print: 2025-12-17

© 2025 Walter de Gruyter GmbH, Berlin/Boston

Articles in the same Issue

  1. Frontmatter
  2. A novel degradation estimation of lifecycle health monitoring for aircraft engine gas path rotational components
  3. Minimum specific fuel consumption performance-seeking control for variable cycle engine based on CHOA-SQP hybrid algorithm and active disturbance rejection control
  4. Effects of splitter blade on vaned-diffuser stall and the corresponding warning method
  5. Uncertainty quantification of leakage characteristics of stepped labyrinth seals based on sparse PC-Kriging model
  6. Uncertainty propagation in transient heat transfer from an extended surface
  7. Impact of mass flow ratio on the aero-thermal performance of a film-cooled nozzle guide vane
  8. Quantification of uncertainty propagation in transient heat transfer from flux-base extended surface
  9. Recent advancements in Scramjet combustor: technologies, fuel strategies, and performance challenges
  10. Deformation and fatigue life analysis of axial flow compressor blade based on fluid-structure interaction
  11. Impact of convex-side blade attachments on savonius vertical axis wind turbines performance at low wind speeds
  12. An energy method for dry friction damping of ring damper in labyrinth seal structure under radial vibration
  13. Uncertainty quantification by probabilistic analysis of Stirling engine performance
  14. Integration of multi module flow domain to demonstrate the full engine aero-flow path simulation of Single Spool Turbojet Engine
  15. Enhancing fuel-air mixing and flame stability using double cavity with multiple struts scramjet propulsion
  16. Investigation on aerodynamic interference mechanism of a contra-rotating propfan under take-off condition
  17. Analysis of the dynamic characteristics of compliant foil gas seal with bearing-rotor system
  18. Investigation of the influence of an S-shaped isolator on the combustion characteristics of a supersonic combustion chamber
  19. Research on adjoint-based customized integrated passage design of Rotor 67
  20. A method for evaluating the time-averaged and unsteady characteristics of flow loss in axial compressors
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