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.
A New High Bypass Fan for General Aviation
Sae Technical Papers
Turbine Powered Executive Aircraft Meeting ; 1980
1980-04-01
Aufsatz (Konferenz)
Englisch
Online Contents | 2009
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NTIS | 1972
Online Contents | 1996