Understanding the Fundamental Roles of Momentum and Vorticity Injections in Flow Control

Abstract

The objective of this study is to numerically investigate the fundamental roles that momentum and vorticity injections play in suppressing flow separation over a canonical airfoil. Open-loop control of separated, incompressible flow over a NACA 0012 airfoil at Re = 23,000 is examined through large-eddy simulations. We find that the modification to the flow field can be captured by quantifying both the effects of wall-normal momentum (coefficient of momentum) and wall-normal vorticity (derived coefficient of circulation), by considering a newly defined total input parameter (total coefficient). Moreover, the study has developed advanced analysis techniques. First, the capability to perform bi-global stability analysis has been developed and validated, which can serve as a basis for physics-based active flow control guided by the knowledge of hydrodynamic instabilities. Second, as part of modeling complex unsteady flows in general, efforts in this study have led to the initial development of a novel network-theoretic approach in quantifying nonlinear interactions present in vortical flows.

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Document Details

Document Type
Technical Report
Publication Date
Sep 02, 2016
Accession Number
AD1016223

Entities

People

  • Aditya Nair
  • Kunihiko Taira
  • Phillip Munday

Organizations

  • Florida State University

Tags

Communities of Interest

  • Energy and Power Technologies
  • Engineered Resilient Systems
  • Space

DTIC Thesaurus Topics

  • Air Force
  • Boundary Layer
  • Computational Fluid Dynamics
  • Computational Science
  • Flow Visualization
  • Fluid Dynamics
  • Fluid Flow
  • Fluid Mechanics
  • Geometry
  • Hydrodynamics
  • Incompressible Flow
  • Mechanics
  • Network Science
  • Reynolds Number
  • Steady Flow
  • Turbulent Flow
  • Turbulent Mixing

Fields of Study

  • Physics

Readers

  • Aerodynamics.
  • Computational Modeling and Simulation
  • Ocean-Atmosphere Mesoscale Modeling, Data Assimilation, and Flux Boundary Layers