Frontmatter

Articles in the same Issue

1. Frontmatter
2. The International Journal of Turbo and Jet Engines
3. The aerothermodynamic cycle optimal design of a turbofan engine
4. Multi-condition design optimization of groove flow control technique in an axial-flow pump
5. Analysis on impulse characteristics of pulse detonation engine with nozzles
6. Numerical investigation on implication of innovative hydrogen strut injector on performance and combustion characteristics in a scramjet combustor
7. Optimization of Kiel geometry for better recovery factor in high temperature measurement in aero gas turbine engine
8. Applicability of correlational data-mining to small-scale turbojet performance map generation
9. Effect of multi-zone effusion cooling on an adiabatic flat plate for gas turbine application
10. Flow quality improvement of the wind tunnel testing for a highly-loaded compressor cascade at high incidence
11. Modeling and analysis of 3D radiative heat transfer in combustor
12. A creep-fatigue life prediction model considering multi-factor coupling effect
13. Optimization-based transient control of turbofan engines: a sequential quadratic programming approach
14. Investigations on the interaction between the front and aft purge flow and the downstream vane of 1.5-stage turbine
15. A study on design optimization for compressor blisks
16. Exploration of an unconventional validation tool to investigate aero engine transonic fan flutter signature
17. Evaluation of non-uniform water film behavior on the performance of an axial aeroengine compressor
18. Predicting remaining useful life of turbofan engines using degradation signal based echo state network
19. Effect of G-type integral squeeze film damper on the dynamic characteristics in rotor system
20. Development of a one-dimensional code for the initial design of a micro gas turbine mixed flow compressor stage
21. Numerical and experimental investigations of tip clearance effects in a high-flow-coefficient centrifugal compressor
22. Experimental and numerical investigation on the effect of turboprop engine exhaust gas impingement on pusher aircraft
23. Heat transfer distribution of single oblique jet impingement in crossflow under different inlet conditions
24. Performance enhancement and flow separation control in an S-duct by air injection
25. Gas dynamic analysis of the modern single shaft gas turbine engine flow path
26. Aero engine health monitoring, diagnostics and prognostics for condition-based maintenance: an overview
27. Influence of leading edge point on aerodynamic performance of asymmetric leading edge compressor airfoils
28. The aerothermal performance of turbine blade squealer tip at various Reynolds numbers and Mach numbers with moving endwall
29. Numerical investigation of a variable stator vane with nonuniform partial radial gaps in an annular compressor cascade
30. Effect of self-recirculating casing treatment on the unsteady flow and stability of counter-rotating axial-flow compressor
31. Research on temperature rise characteristics of end V-groove ring seal
32. Research on the influence of honeycomb cell blockage on the seal leakage characteristics
33. Vortex structure control based bleed in axial compressor cascade with tip clearance using large eddy simulation
34. Development and application of a profile loss model considering the low-Re effect in low-pressure turbine
35. Optimization of ACE mode transition control schedule considering geometric adjustment speed
36. Numerical investigation of flow control in low-pressure turbine cascade using Gurney Flaps
37. The design method of the V-shaped groove piston ring
38. Control of subsonic jets using vanes as vortex generators
39. Impact investigation of inlet environmental changes on the rated condition performance of a high-pressure compressor
40. Research on new integral squeeze film damper vibration control of micro turbojet engine at high speed
41. Effect of the distribution of the upstream probe support on performance of compressor cascade
42. Effect of bypass ratio on sonic underexpanded co-flow jets with finite lip thickness
43. Machine learning augmented multi-sensor data fusion to detect aero engine fan rotor blade flutter
44. CFD analysis of flow control in compressor cascade using MVGs
45. Quantitative investigation of the evaporation and resistance characteristics of inlet jet precooling
46. Study on laser de-weight and dynamic balance technology of rotating machines
47. Integrated design and analysis of inlet and missile with two side layout
48. Research on turboprop engine control method based on linear parameter varying model
49. Modeling and validation of the volume effect on the axial fan transient performance
50. Ground effects on the aerodynamics of a wing with slot type distributed propulsion system for VTOL applications
51. Multidisciplinary sensitivity analysis for turbine blade considering thickness uncertainties
52. Accurate measurement and evaluation method of axial compressor efficiency under the influence of multiple factors
53. Control mechanism of secondary flow in a turbine cascade with non-axisymmetric endwall profiling under Co-rotating incoming vortex
54. Infrared simulation of aircraft rear fuselage based on a coupled CFD method
55. Effect of multi-hole trench cooling on an adiabatic flat plate for gas turbine application
56. Numerical study of transition process in different zones of a compressor cascade channel