Blade Sections in Streamwise Oscillations into Reverse Flow

F-0071-2015-10273

5/5/2015

Authors
Abstract
Content
ABSTRACT

A low-Reynolds number rectilinear analog of the retreating blade problem is considered by computationally and experimentally studying a NACA0012 blade in spanwise oscillation in a free stream. Three-dimensional hybrid RANS-LES simulations with spanwise periodic boundary conditions and experimental flow visualization support the description of experimental direct force measurements for a wide range reduced frequencies and advance ratios, including fully reversed flow conditions. A fixed incidence of 6 degrees is taken as a nominally attached-flow case, and agrees reasonably well with Isaacs' theory. A fixed incidence of 20 degrees is taken as a fully-separated case, and departs markedly from inviscid theory, and even more so from quasi-steady approximation. Experimental-computational comparison shows a computational overprediction of lift relative to experimental results, at moderate advance ratios. Agreement in fully reversed flow is, however, quite good.

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DOI
https://doi.org/10.4050/F-0071-2015-10273
Citation
Ol, M., Granlund, K., Jones, A., Mulleners, K., et al., "Blade Sections in Streamwise Oscillations into Reverse Flow," Vertical Flight Society 71st Annual Forum and Technology Display, Virginia Beach, Virginia, May 5, 2015, https://doi.org/10.4050/F-0071-2015-10273.
Additional Details
Publisher
Published
5/5/2015
Product Code
F-0071-2015-10273
Content Type
Technical Paper
Language
English