Frontmatter

Articles in the same Issue

1. Frontmatter
2. Numerical investigations of heat transfer characteristics using oblong fins and circular fins in a wedge channel
3. An efficient flow control technique based on co-flow jet and multi-stage slot circulation control applied to a supercritical airfoil
4. Reacting flow analysis in scramjet engine: effect of mass flow rate of fuel and flight velocity
5. Installed performance seeking control based on supersonic variable inlet/engine coupling model
6. Effect of zero penetration angle chevrons in supersonic jet noise and screech tone mitigation
7. The aerodynamic performance degradation analysis of a small high bypass turbofan engine compression system with fan rotor blade leading edge erosion
8. Flow structure comparison of film cooling versus hybrid cooling: a CFD study
9. Experimental investigation on a Jeffcott rotor with combined coupling misalignment using time-frequency analysis
10. Effect of free boundary on the performance of single expansion nozzle
11. Optimization and numerical investigation of combined design of blade and endwall on rotor 67
12. Numerical study on the effect of distortion of S-duct on flow field and performance of a full annulus transonic fan
13. Research on a high-precision real-time improvement method for aero-engine component-level model
14. Uncertainty quantification by probabilistic analysis of circular fins
15. Influences of unbalance phase combination on the dynamic characteristics for a turboprop engine
16. Study on the water ingestion performance of compressor with inlet particle separator
17. The role of volume effect on the transient behavior of a transonic compressor
18. Experimental analysis of performance and tip dynamic pressure in a compressor cascade with high-speed moving endwall
19. Numerical study of the impact of hydrogen addition, swirl intensity and equivalence ratio on methane-air combustion
20. Active subspace-based performance analysis of supersonic through-flow fan rotor
21. Assessment of performance degradation of a mixed flow low bypass turbofan engine through GasTurb simulation
22. Numerical investigation of tip clearance flow in a variable geometry turbine with non-uniform partial clearance