Frontmatter

Articles in the same Issue

1. Frontmatter
2. Characterization of titanium grade 5 alloy compressor blade in a jet engine using advanced materials for optimum thrust production
3. Numerical investigation of total temperature distortion problem in a multistage fan based on body force approach
4. Life assessment of a high temperature probe designed for performance evaluation and health monitoring of an aero gas turbine engine
5. Baseline architecture design for a turboelectric distributed propulsion system using single turboshaft engine operational scenario
6. Active fault tolerant control of turbofan engines with actuator faults under disturbances
7. Modeling and mode transition simulation of over-under turbine based combined cycle (TBCC) propulsion system based on inlet/engine matching
8. Numerical analysis of high temperature gas flow through conical micronozzle
9. Simulation and analysis of an aero-engine combustor with a slinger fuel injection system
10. Influence of plasma-chemical products on process stability in a low-emission gas turbine combustion chamber
11. Influence of nozzle exit geometrical parameters on supersonic jet decay
12. Experimental investigation on mixing characteristics of high speed co-flow jets by using tabbed chevron nozzle
13. Study of a new effervescent atomizer design