NASA NTRS · 19890000466
Interaction Of A Helicopter Blade With A Vortex
Abstract
Measurements in wind tunnel yield data for validation of computations. Report describes experimental investigation of three-dimensional interaction of helicopter rotor blade with vortex like that generated by preceeding rotor blade. Provides theoretical aerodynamicists with data for validation of computer simulations of aerodynamic flow.
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Dunagan, Stephen, Norman, Thomas. 1989-09-01. Interaction Of A Helicopter Blade With A Vortex. https://ntrs.nasa.gov/citations/19890000466
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