A Reynolds Number‐Based Blade Tip Vortex Model
Abstract:A mathematical model has been developed to estimate the temporal growth properties of helicopter blade tip vortices at any vortex Reynolds number. The uniqueness of the model is that it takes into account rotational stratification (Richardson number) effects on the distribution of turbulent viscosity inside the tip vortices. This model is combined with the effects of filament stretching in predicting the temporal evolution of the vortex. A turbulent growth model solves exactly for the tangential (swirl) velocity starting from the Navier‐Stokes equations by using a variation in eddy viscosity across the vortex core. This variation is a function of the local Richardson number, and the final solution becomes dependent on vortex Reynolds number. A parsimonious functional approximation is given to represent the induced velocity distribution in the tip vortices for practical applications. It is shown that the temporal core growth rate predicted by the new model increases with an increase in vortex Reynolds number, which is consistent with experimental observations. The predictions from the model were validated, wherever possible, with tip vortex measurements from both model‐scale and full‐scale rotors.
Document Type: Research Article
Affiliations: Alfred Gessow Rotorcraft Center, Department of Aerospace Engineering, Glenn L. Martin Institute of Technology, University of Maryland, College Park, MD
Publication date: July 1, 2007
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