Blade Sections in Streamwise Oscillations into Reverse Flow

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 over-prediction of lift relative to experimental results, at moderate advance ratios. Agreement in fully reversed flow is, however, quite good.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
May 07, 2015
Accession Number
ADA636818

Entities

People

  • Anya R. Jones
  • Joachim Hodara
  • Karen Mulleners
  • Kenneth Granlund
  • Marilyn Smith
  • Michael Ol

Organizations

  • Georgia Tech Research Corporation

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Air Force
  • Air Force Research Laboratories
  • Aircrafts
  • Airframes
  • Boundary Layer
  • Dynamic Pressure
  • Flow Visualization
  • Fluid Dynamics
  • Fluid Flow
  • Helicopters
  • Military Research
  • Reynolds Number
  • Rotary Wing Aircraft
  • Short Takeoff Aircraft
  • Three Dimensional
  • Turbulent Mixing

Fields of Study

  • Physics

Readers

  • Aerodynamics.
  • Computational Fluid Dynamics (CFD)
  • Fluid Mechanics and Fluid Dynamics.