Article
Publicly Available
Frontmatter
Published/Copyright:
December 1, 2025
Published Online: 2025-12-01
Published in Print: 2025-12-17
© 2025 Walter de Gruyter GmbH, Berlin/Boston
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Articles in the same Issue
- Frontmatter
- A novel degradation estimation of lifecycle health monitoring for aircraft engine gas path rotational components
- Minimum specific fuel consumption performance-seeking control for variable cycle engine based on CHOA-SQP hybrid algorithm and active disturbance rejection control
- Effects of splitter blade on vaned-diffuser stall and the corresponding warning method
- Uncertainty quantification of leakage characteristics of stepped labyrinth seals based on sparse PC-Kriging model
- Uncertainty propagation in transient heat transfer from an extended surface
- Impact of mass flow ratio on the aero-thermal performance of a film-cooled nozzle guide vane
- Quantification of uncertainty propagation in transient heat transfer from flux-base extended surface
- Recent advancements in Scramjet combustor: technologies, fuel strategies, and performance challenges
- Deformation and fatigue life analysis of axial flow compressor blade based on fluid-structure interaction
- Impact of convex-side blade attachments on savonius vertical axis wind turbines performance at low wind speeds
- An energy method for dry friction damping of ring damper in labyrinth seal structure under radial vibration
- Uncertainty quantification by probabilistic analysis of Stirling engine performance
- Integration of multi module flow domain to demonstrate the full engine aero-flow path simulation of Single Spool Turbojet Engine
- Enhancing fuel-air mixing and flame stability using double cavity with multiple struts scramjet propulsion
- Investigation on aerodynamic interference mechanism of a contra-rotating propfan under take-off condition
- Analysis of the dynamic characteristics of compliant foil gas seal with bearing-rotor system
- Investigation of the influence of an S-shaped isolator on the combustion characteristics of a supersonic combustion chamber
- Research on adjoint-based customized integrated passage design of Rotor 67
- A method for evaluating the time-averaged and unsteady characteristics of flow loss in axial compressors