An Experimental Investigation of High Subsonic Flow Over an Off Axis Longitudinal Cavity with Antiresonance Devices

Abstract

This study is a preliminary effort to reduce the level of the resonance and to provide a means of predicting the pressure gains and resonant frequencies associated with a forward facing cylindrical cavity in high subsonic flow. The basic model was an ogive cylinder fitted with an off-axis longitudinal cavity. Eleven different suppression devices were investigated. Transmission line theory was used very effectively to predict the pressure gains and resonant frequency when the flow was stagnated in the cavity and to predict the resonant frequency in flow situations. The resonant frequency occurred at or near the fundamental mode frequency of a right circular cavity. The most effective anti- resonance device, a side relief hole, reduced the RMS pressure in the cavity by a factor as great as 23. Helmholtz resonators placed in the cavity were also shown to be effective, reducing the RMS pressure by a factor as great as 6.

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Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1974
Accession Number
ADA023352

Entities

People

  • Kenneth Vaccaro

Organizations

  • Air Force Institute of Technology

Tags

Communities of Interest

  • Advanced Electronics
  • Air Platforms

DTIC Thesaurus Topics

  • Abstracts
  • Air Force
  • Aircrafts
  • Computer Programs
  • Correlators
  • Engineering
  • Frequency
  • Frequency Response
  • Governments
  • Mach Number
  • Plastic Explosives
  • Pressure Measurement
  • Pressure Transducers
  • Resonance
  • Resonant Frequency
  • Resonators
  • Transducers

Fields of Study

  • Physics

Readers

  • Acoustics.
  • Electromagnetic Wave Scattering and Antenna Radiation Engineering
  • Fluid Dynamics.