Analysis of Cavity Passive Flow Control High Speed Shadowgraph Images (Postprint)

Abstract

An examination of a rectangular cavity with an L/D of 5.67 was tested at Mach 0.7 with a corresponding Reynolds number of 2x10(exp 6)/ft. High speed shadowgraph movies were simultaneously sampled with dynamic pressure sensors at 75 kHz. Fourier analysis was performed on the high speed movies as well as the dynamic pressure data, which resulted in determining the locations of dominant cavity frequencies in the flow field. Five passive flow control devices were tested, three of which have historically preformed well, while two neither reduced the main acoustic tones nor reduced the broadband levels. From the high speed shadowgraph movies, observations are made in the changes in the cavity flow physics when the passive flow control devices are used, and will be discussed.

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Document Details

Document Type
Technical Report
Publication Date
Dec 01, 2011
Accession Number
ADA579373

Entities

People

  • Anwar Ahmed
  • Frank Semmelmayer
  • James E. Grove
  • Mitchell Haverkamp
  • Ryan F. Schmit

Organizations

  • Air Force Research Laboratory

Tags

Communities of Interest

  • Sensors
  • Space

DTIC Thesaurus Topics

  • Acoustics
  • Acquisition
  • Air Force
  • Boundary Layer
  • Computational Fluid Dynamics
  • Data Acquisition
  • Dynamic Pressure
  • Flow Fields
  • Fluid Dynamics
  • Fluid Flow
  • Fluid Mechanics
  • Frequency
  • Frequency Shift
  • Hypervelocity Flow
  • Physics Laboratories
  • Reynolds Number
  • Turbulent Mixing

Readers

  • Acoustics.
  • Combustion and Flow Dynamics.
  • Image Processing and Computer Vision.