Performance Assessment of the Thermodynamic Cycle in a Multi-Mode Gas Turbine Engine
This chapter discusses the direction of development of promising multimode aviation gas turbine engines (GTE). It is shown that the development of GTE is on the way to increase the parameters engine workflow: gas temperatures in front of the turbine (T*G) and the degree of pressure increase in the c...
Guardado en:
| Autores principales: | , |
|---|---|
| Formato: | Capítulo de libro |
| Lenguaje: | inglés |
| Publicado: |
IntechOpen
2021
|
| Materias: | |
| Acceso en línea: | https://www.intechopen.com/chapters/76346 |
| Etiquetas: |
Sin Etiquetas, Sea el primero en etiquetar este registro!
|
Ejemplares similares: Performance Assessment of the Thermodynamic Cycle in a Multi-Mode Gas Turbine Engine
- Biofuel and Gas Turbine Engines
- Titanium in the Gas Turbine Engine
- Micro Gas Turbine Engine: A Review
- Retracted: The Selection of Materials for Marine Gas Turbine Engines
- Influence of Heat Transfer on Gas Turbine Performance
- Synthesis of Flow Simulation Methods for Fast and Accurate Gas Turbine Engine Performance Estimation