Blade Sections in Streamwise Oscillations into Reverse Flow
F-0071-2015-10273
5/5/2015
- Content
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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.
- 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.