Wind tunnel simulation tests are reported that utilize a 20 inch powered nacelle for airframe integration studies. Considered are: effects of boattail positioning, nacelle size, aft fuselage drag, over-the-wing half span model installation, and turboprop and ducted fan configurations.
Propulsion airframe integration
1975-01-01
Aufsatz (Konferenz)
Keine Angabe
Englisch
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