ACOUSTIC ADMITTANCE OF BURNING SOLID PROPELLANT SURFACE.

Abstract

Progress is being made in perfecting the proposed single pulse method to a point where it can be employed to obtain the admittance-frequency curve for assorted materials (without combustion in this initial phase of the study). A spark is used to generate a weak shock wave which becomes planar in its travel down a long tube of rectangular cross section. At the end of the tube the wave meets the surface of the solid being tested and is reflected back up the tube. A transducer flushmounted in the tube picks up the pressure-time profiles of the incident and reflected waves. This information in the form of photographs of the oscilloscope traces is used in the machine calcution of the complex acoustic admittance.

Document Details

Document Type
Technical Report
Publication Date
Jun 30, 1961
Accession Number
AD0609885

Entities

Organizations

  • SRI International

Tags

DTIC Thesaurus Topics

  • Acoustic Admittance
  • Combustion
  • Energetic Materials
  • Frequency
  • Frequency Shift
  • Materials
  • Oscilloscopes
  • Photographs
  • Photography
  • Propellants
  • Shock
  • Shock Waves
  • Solid Propellants
  • Waves

Fields of Study

  • Physics

Readers

  • Combustion Dynamics and Shock Wave Physics.
  • Electromagnetic Wave Scattering and Antenna Radiation Engineering