An Investigation of the Reacting and Non-Reacting Flow Characteristics of Solid Fuel Ramjets.

Abstract

An investigation was conducted to determine the relationship between the non-reacting and the reacting flow characteristics of solid fuel ramjets. Polymethylmethacrylate fuel grains were burned in a ramjet motor on a thrust stand. Combustion efficiency, regression rate profile and pressures were determined for the reacting flows and compared to profiles obtained in non-reacting flows for velocity, pressure, and near-wall and centerline turbulence intensity. Near-wall turbulence profiles were in agreement with the fuel regression profiles obtained in reacting flows. Combustion efficiency was found to be a strong function of mixture ratio. Near-wall mixing significantly increased fuel regression rate. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1980
Accession Number
ADA094567

Entities

People

  • Winston Elliott Scott

Organizations

  • Naval Postgraduate School

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Supplies
  • Calibration
  • Combustion
  • Data Acquisition
  • Diameters
  • Efficiency
  • Fuels
  • Geometry
  • Ignition
  • Intensity
  • Mach Number
  • Measurement
  • Plastic Explosives
  • Pressure Distribution
  • Secondary Flow
  • Solid Fuels
  • Turbulence

Fields of Study

  • Physics

Readers

  • Fluid Mechanics and Fluid Dynamics.
  • Rocket Propulsion.