Frontmatter

Articles in the same Issue

1. Frontmatter
2. Integration of a transonic high-pressure turbine with a rotating detonation combustor and a diffuser
3. Prediction of compressor nominal characteristics of a turboprop engine using artificial neural networks for build standard assessment
4. Study on inversion control for integrated helicopter/engine system with variable rotor speed based on state variable model
5. Effects of casing angle on the performance of parallel hub axial annular diffuser
6. Experimental research on the performance of the forward variable area bypass injector for variable cycle engines
7. Film cooling characteristics on a grooved surface with different injection orientation angles
8. Aero-thermal optimization of the rim seal cavity to enhance rotor platform thermal protection
9. Numerical study of the parameters of a gas turbine combustion chamber with steam injection operating on distillate fuel
10. An active fault-tolerant control strategy of aircraft engines based on multi-model predictive control
11. Conjugate heat transfer analysis of a radially cooled nozzle guide vane in an aero gas turbine engine
12. A new method to improve the real-time performance of aero-engine component level model
13. Experimental and numerical investigation of expansion corner effects on isolator performance