Frontmatter

Articles in the same Issue

1. Frontmatter
2. Proper Orthogonal Decomposition analysis of mode switching in supersonic jets impinging on flat and corrugated plates
3. Impact of cavity and ramp configuration on the combustion performance of a strut-based scramjet combustor
4. In-service load calculation surrogate models for high-pressure turbine blade life digital twin
5. Numerical analysis on the effect of passive control geometry in supersonic jet mixing enhancement
6. Study on one-dimensional performance prediction of multi-stage axial turbine based on the blade height
7. Dynamic characteristics of open-ends squeeze film dampers with air ingestion
8. Fluid flow in a microdiffuser at small Reynolds numbers
9. A study on optimal rotor speed control method for helicopter power system considering the influence of infrared suppressors
10. Effects of turbulence and flamelet combustion modelling on the CFD simulation of a dual inlet ramjet combustor
11. Design and combustion characteristics analysis of a static shaft turbofan engine
12. Aerothermal effects of squealer openings on a cavity tip in a turbine cascade
13. Endwall heat transfer in wedge channel with teardrop pin fins, circular fins and oblong pin fins
14. Virtual deflection with synthetic jet actuators at high angles of attack
15. Design of mode transition control system for tandem TBCC engine based on direct performance parameters closed-loop control
16. Effect of tab shape, length, and placement on the over-expanded free jet at Mach 2.0
17. Influence of the ending position of controllable speed casing on a transonic compressor rotor tip leakage flow
18. Integrated modeling and coupling characteristics analysis of helicopter/engine/infrared suppressor
19. Effect of velocity ratio and Mach number on thin lip coaxial jet
20. C conjugate heat transfer simulation of swirl internal cooling on blade leading edge
21. Influence of inlet structure on combustion flow structure in magnesium powder fueled water ramjet engine
22. Research on high-bandwidth linear active disturbance rejection control method for variable speed turboshaft engine
23. Numerical investigation of force over the horizontal jet tab of various sector angle fixed to the convergent-divergent nozzle exit