Frontmatter.
- Published in:
- International Journal of Turbo & Jet-Engines, 2025, v. 42, n. 2, p. i, doi. 10.1515/tjj-2025-frontmatter2
- Publication type:
- Article
Works matching IS 03340082 AND DT 2025 AND VI 42 AND IP 2
Results: 20
1
2
Flight trajectory optimization study of a variable-cycle turbine-based combined cycle engine hypersonic vehicle based on airframe/engine integration.
- Published in:
- International Journal of Turbo & Jet-Engines, 2025, v. 42, n. 2, p. 409, doi. 10.1515/tjj-2024-0085
- By:
- Publication type:
- Article
3
Constant temperature line identification on prototype gas turbine combustor with multi-colour change coating.
- Published in:
- International Journal of Turbo & Jet-Engines, 2025, v. 42, n. 2, p. 423, doi. 10.1515/tjj-2024-0083
- By:
- Publication type:
- Article
4
Sensitivity analysis of aero-engine performance optimization control system and its hardware test verification.
- Published in:
- International Journal of Turbo & Jet-Engines, 2025, v. 42, n. 2, p. 433, doi. 10.1515/tjj-2024-0082
- By:
- Publication type:
- Article
5
Flow pattern formation due to the interdependency of multi-component interactions and their impact on the performance of turbine and exhaust duct of gas turbine.
- Published in:
- International Journal of Turbo & Jet-Engines, 2025, v. 42, n. 2, p. 397, doi. 10.1515/tjj-2024-0079
- By:
- Publication type:
- Article
6
Numerical analysis of brush seal hysteresis based on orthogonal test method.
- Published in:
- International Journal of Turbo & Jet-Engines, 2025, v. 42, n. 2, p. 367, doi. 10.1515/tjj-2024-0078
- By:
- Publication type:
- Article
7
Thermal performance of teardrop pin fins and zig zag ribs in a wedge channel.
- Published in:
- International Journal of Turbo & Jet-Engines, 2025, v. 42, n. 2, p. 293, doi. 10.1515/tjj-2024-0071
- By:
- Publication type:
- Article
8
Investigation of varying tip clearance gap and operating conditions on the fulfilment of low-speed axial flow fan.
- Published in:
- International Journal of Turbo & Jet-Engines, 2025, v. 42, n. 2, p. 305, doi. 10.1515/tjj-2024-0067
- By:
- Publication type:
- Article
9
Speed controller design for turboshaft engine using a high-fidelity AeroThermal model.
- Published in:
- International Journal of Turbo & Jet-Engines, 2025, v. 42, n. 2, p. 347, doi. 10.1515/tjj-2024-0060
- By:
- Publication type:
- Article
10
Determination of the modern marine single shaft gas turbine rotor blades fatigue strength parameters.
- Published in:
- International Journal of Turbo & Jet-Engines, 2025, v. 42, n. 2, p. 271, doi. 10.1515/tjj-2024-0057
- By:
- Publication type:
- Article
11
Multi-nozzle thrust matching control of STOVL engine.
- Published in:
- International Journal of Turbo & Jet-Engines, 2025, v. 42, n. 2, p. 355, doi. 10.1515/tjj-2024-0054
- By:
- Publication type:
- Article
12
Compensator based improved model predictive control for Aero-engine.
- Published in:
- International Journal of Turbo & Jet-Engines, 2025, v. 42, n. 2, p. 447, doi. 10.1515/tjj-2024-0052
- By:
- Publication type:
- Article
13
Conjugated heat transfer characteristics of ribbed-swirl cooling in turbine blade under rotation condition.
- Published in:
- International Journal of Turbo & Jet-Engines, 2025, v. 42, n. 2, p. 381, doi. 10.1515/tjj-2024-0046
- By:
- Publication type:
- Article
14
Review of gliding arc plasma assisted ignition and combustion for gas turbine application.
- Published in:
- International Journal of Turbo & Jet-Engines, 2025, v. 42, n. 2, p. 241, doi. 10.1515/tjj-2024-0045
- By:
- Publication type:
- Article
15
Role of different cavity flame holders on the performance characteristics of supersonic combustor.
- Published in:
- International Journal of Turbo & Jet-Engines, 2025, v. 42, n. 2, p. 277, doi. 10.1515/tjj-2024-0037
- By:
- Publication type:
- Article
16
Deep residual ensemble model for predicting remaining useful life of turbo fan engines.
- Published in:
- International Journal of Turbo & Jet-Engines, 2025, v. 42, n. 2, p. 229, doi. 10.1515/tjj-2024-0025
- By:
- Publication type:
- Article
17
Performance evaluation of a scramjet engine utilizing varied cavity aft wall divergence with parallel injection in a reacting flow field.
- Published in:
- International Journal of Turbo & Jet-Engines, 2025, v. 42, n. 2, p. 331, doi. 10.1515/tjj-2024-0020
- By:
- Publication type:
- Article
18
Upgraded one-dimensional code for the design of a micro gas turbine mixed flow compressor stage with various crossover diffuser configurations.
- Published in:
- International Journal of Turbo & Jet-Engines, 2025, v. 42, n. 2, p. 317, doi. 10.1515/tjj-2024-0016
- By:
- Publication type:
- Article
19
Interaction effects between the rotor wake and hub leakage flow in a multi-stage cantilevered compressor.
- Published in:
- International Journal of Turbo & Jet-Engines, 2025, v. 42, n. 2, p. 261, doi. 10.1515/tjj-2023-0003
- By:
- Publication type:
- Article
20
Ignition experimental study based on rotating gliding arc.
- Published in:
- International Journal of Turbo & Jet-Engines, 2025, v. 42, n. 2, p. 459, doi. 10.1515/tjj-2022-0041
- By:
- Publication type:
- Article