General Considerations in the Design of Combustion Chambers for Aircraft and Industrial Gas Turbines Joseph Lucas, Limited

Format:

Conference/Event

Author/Creator:

Clarke, J. S., author.

Conference Name:

SAE World Congress & Exhibition (1964-01-01 : Detroit, Michigan, United States)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1964

Summary:

AbstractThis paper reviews those requirements that are common in the design of all gas turbines combustion equipment. Where necessary, a distinction is made between the demands of industrial and aircraft chambers. The problem of designing equipment for long life and low pressure loss, in a size compatible with the overall engine, is discussed in detail, and the application of combustor characteristics and design factors to the demands of new aircraft and industrial turbines are anticipated

Notes:

Vendor supplied data

Publisher Number:

640009

Access Restriction:

Restricted for use by site license