The Onset of Dynamic Stall: Understanding Flowfield Unsteadiness to Enable Closed-Loop Control

Abstract

The current study was conducted in order to characterize the quantitative spatiotemporal scales associated with the dynamic stall flow field across a transitional-Reynolds number regime. Across these higher Reynolds numbers, a series of flow field interactions were observed to produce a broad distribution of scales not observed in the canonical dynamic stall process at lower Reynolds numbers from the literature. From this study, unsteady flow oscillations associated with a laminar separation bubble were identified. These oscillations emerged prior to the inception of the dynamic stall process, and were observed to follow a Strouhal number scaling of 1.2, when the separation bubble height was used as the characteristic length scale. Further study of the off-body velocity field revealed variations in the developmental morphology of the dynamic stall vortex with changing Reynolds number. An Empirical Mode Decomposition method was coupled to a Hilbert spectral analysis method to provide a quantitative characterization of the temporal scales that emerge during unsteady separation and dynamic stall vortex formation.

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Document Details

Document Type
Technical Report
Publication Date
Apr 19, 2019
Accession Number
AD1085947

Entities

People

  • Phillip J. Ansell

Tags

Communities of Interest

  • Energy and Power Technologies
  • Human Systems
  • Materials and Manufacturing Processes

DTIC Thesaurus Topics

  • Air Force Research Laboratories
  • Boundary Layer
  • Flow
  • Flow Fields
  • Fluid Dynamics
  • Fluid Flow
  • Frequency
  • Military Research
  • Physics
  • Physics Laboratories
  • Pressure Distribution
  • Pressure Measurement
  • Reynolds Number
  • Stratified Fluids
  • Strouhal Number
  • Turbulent Mixing
  • Unsteady Flow

Fields of Study

  • Physics

Readers

  • Fluid Mechanics and Fluid Dynamics.
  • Systems Analysis and Design