NASA NTRS · 19930045440
Recent developments in rotor wake modeling for helicopter noise prediction
Abstract
A preliminary test/theory correlation evaluation is conducted for wake measurement test results obtained by LDV for a B360 helicopter rotor, at conditions critical to the understanding of wake-rollup and blade-vortex interaction phenomena. The LDV data were complemented by acoustic, blade pressure, rotor performance, and blade/control load measurements.
Keep this discovery
Explore connections, maps & timelines
Poling, D., Dadone, L., Althoff, S.. 1991-01-01. Recent developments in rotor wake modeling for helicopter noise prediction. https://ntrs.nasa.gov/citations/19930045440
Cite the original work for its findings. Save a collection to share your selection of sources.