NASA NTRS · 19760003938
Propulsion airframe integration
Abstract
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.
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Mikkelson, D.. 1975-01-01. Propulsion airframe integration. https://ntrs.nasa.gov/citations/19760003938
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