A New High Bypass Fan for General Aviation

Format:

Conference/Event

Author/Creator:

Schrader, J.W., author.

Conference Name:

Turbine Powered Executive Aircraft Meeting (1980-04-09 : Scottsdale, Arizona, United States)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1980

Summary:

A small, high bypass turbofan engine, suitable for use in general aviation aircraft, was designed, built and tested. Key features of the engine include low noise, low exhaust emissions and high propulsive efficiency. Testing was conducted with a simulated flight nacelle. Exhaust emissions were measured and the noise data taken was used to predict sideline, takeoff and approach noise levels

Notes:

Vendor supplied data

Publisher Number:

800602

Access Restriction:

Restricted for use by site license