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

Format:

Conference/Event

Author/Creator:

Viall, W. S., 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:

Consideration is given the manner in which inlet throat Mach number. cowl forebody lip suction loss, boattail pressure, and skin friction affect the design of nacelles for high bypass ratio, short duct engines. The mutual relationship of the fan nozzle, hot gas nozzle, the gas generator cowling, and the fan cowl is discussed

Notes:

Vendor supplied data

Publisher Number:

660733

Access Restriction:

Restricted for use by site license