Integration effects of underwing forward- and rearward-mounted separate-flow, flow-through nacelles on a high-wing transport

An edition of Integration effects of underwing forward- and rearward-mounted separate-flow, flow-through nacelles on a high-wing transport (1986)

Integration effects of underwing forward- and rearward-mounted separate-flow, flow-through nacelles on a high-wing transport

By Milton Lamb

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Publish Date

1986

Publisher

National Aeronautics and Space Administration, Scientific and Technical Information Branch,For sale by the National Technical Information Service

Language

eng

Pages

Description:

subjects: Nacelles, Skin friction, Pylons, System effectiveness, Wind tunnel tests, Testing, Airplanes, Aerodynamic drag, Transonic planes, Wings