Aerodynamic Considerations for Engine Exhaust Design for Subsonic High Bypass Fan Engines Commercial Airplane Div., The Boeing Company

Format:

Conference/Event

Author/Creator:

Frazier, G. T., author.

Conference Name:

National Aeronautic and Space Engineering and Manufacturing Meeting (1966-10-03 : Los Angeles, California, United States)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1966

Summary:

Analytically and empirically derived external and internal aerodynamic data have been applied to the high-speed cruise development of a low-drag, minimum thrust loss, strut mounted nacelle. The nacelle considered for this study houses a high bypass ratio subsonic fan engine with a short fan duct and a primary plug nozzle. The analysis technique has been geared to a simple geometric description of the nacelle and exhaust system so that high-speed computers may be used to generate trade data. The trade data permit the selection of exhaust systems which, when combined with the complete nacelle, will provide the highest thrust-minus-drag configuration consistent with the airplane cruise mission

Notes:

Vendor supplied data

Publisher Number:

660734

Access Restriction:

Restricted for use by site license