Name: Numerical Analysis and Optimization of the Ultra Compact Combustor (en Inglés)
SKU: 59803280
Price: 518.23 MXN
Availability: InStock
Author: Greenwood, Roger T.
ISBN: 9781288313419

portada Numerical Analysis and Optimization of the Ultra Compact Combustor (en Inglés)

Numerical Analysis and Optimization of the Ultra Compact Combustor (en Inglés)

Formato

Libro Físico

Autor

Roger T. Greenwood

Editorial

Biblioscholar

Idioma

Inglés

N° páginas

102

Encuadernación

Tapa Blanda

Dimensiones

24.6x18.9x0.5 cm

Peso

0.20 kg.

ISBN13

9781288313419

Categorías

Educación

Numerical Analysis and Optimization of the Ultra Compact Combustor (en Inglés)

Roger T. Greenwood (Autor) · Biblioscholar · Tapa Blanda

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Reseña del libro "Numerical Analysis and Optimization of the Ultra Compact Combustor (en Inglés)"

In an effort to increase thrust per weight ratio and decrease pollutant emissions of aero-turbine jet engines, a circumferentially burning Ultra Compact Combustor (UCC) with a Cavity-in-a-Cavity design has been developed. A numerical analysis of this design has been conducted and compared with experimental results. The CFD model has been validated through a wide range of conditions and four alternative physical configurations of the UCC have been modeled. Emissions, combustor efficiencies, temperature and velocity profiles, and pressure drop values were used as comparison parameters. Numerical results indicate that increasing the outflow area will increase the pressure drop over the combustor and decrease the combustor efficiency. A significant decrease (250%) in the cavity circumferential velocity effectively decreased the fuel-air mixing in the cavity resulting in decreased combustion efficiencies. A decreased cavity length reduced combustor pressure drop significantly with only minimal increases in pollutant emissions. The addition of a curved vane to the decreased cavity length configuration further decreased the pressure drop.