Development of the JT15D-1 Turbofan Engine

Format:

Conference/Event

Author/Creator:

Cook, D. L., author.

Conference Name:

National Business Aircraft Meeting and Engineering Display (1972-03-15 : Wichita, Kansas, United States)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1972

Summary:

The UACL JT15D-1 engine is a 2200 lb thrust turbofan engine of the high bypass ratio type, the first small engine of the type to be certified and placed in production. The engine is briefly described, and the scope of development testing and resources applied is reviewed. A selection of major development problems is covered, and future developments are indicated

Notes:

Vendor supplied data

Publisher Number:

720352

Access Restriction:

Restricted for use by site license