Nonlinear Interaction Between Acoustics and Propellant Combustion.

Abstract

This report results from a contract tasking Dipanmento Di Ingegneria Aerospaziale as follows: The contractor will review Russian works on response function of solid propellant combustion to oscillatory pressure and on acoustic admittance. Differences and similarities between US and Russian approaches to this problem shall be considered.

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Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1996
Accession Number
ADA320802

Entities

People

  • Boris V. Novozhilov

Organizations

  • University of Turin

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Acoustic Admittance
  • Acoustics
  • Burning Rate
  • Chemical Reactions
  • Combustion
  • Combustion Chambers
  • Combustion Products
  • Equations
  • Experimental Data
  • Frequency
  • Heat Transfer
  • Integral Equations
  • Propellants
  • Solid Propellants
  • Steady State
  • Surface Temperature
  • Temperature Gradients

Fields of Study

  • Physics

Readers

  • Combustion science or combustion engineering.
  • Electromagnetic Wave Scattering and Antenna Radiation Engineering
  • Technical Research and Report Writing.