NASA NTRS · 19840000328
Over-the-Wing Propeller Reduces Wing Drag
Abstract
Airflow favorably altered if propeller placed above and behind wing. Relocating propeller induces flow over wing airfoil leading edge, which produces leading-edge suction forces not usually attainable by wing in free-stream flow. Concept reduced drag significantly on aircraft model in 12-foot (3.7-meter) wind tunnel. Relocation also helps to reduce cabin noise.
Keep this discovery
Explore connections, maps & timelines
Johnson, J. L., Jr., White, R.. 1985-04-01. Over-the-Wing Propeller Reduces Wing Drag. https://ntrs.nasa.gov/citations/19840000328
Cite the original work for its findings. Save a collection to share your selection of sources.