Raman Scattering Study of Supercritical Bi-Component Mixtures Injected into a Subcritical Environment

Abstract

This research studies the species distribution profiles of methane/ethylene bi-components at downstream locations filled with subcritical nitrogen in a closed chamber. Unique thermodynamic and transport properties of supercritical fluids along with phase transition phenomena during fuel injection process can significantly change combustion characteristics inside a scramjet combustor. Plume properties of supercritical jets are of great interests to the studies of fuel/air mixing and subsequent combustion. The primary goal of this research is to help to clarify whether there is any preferential condensation within the condensed jets. The Raman Scattering technique is used to quantify spatial distribution of injected methane and ethylene. Each species distribution profile is developed in terms of mole fraction. Results demonstrated there is ethylene preferential condensation within the supercritical bi-component mixture of the jet. It also showed the condensation phenomenon is less desirable for combustion. 15.

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Document Details

Document Type
Technical Report
Publication Date
Sep 01, 2007
Accession Number
ADA474331

Entities

People

  • Young M. An

Organizations

  • Air Force Institute of Technology

Tags

Communities of Interest

  • Advanced Electronics
  • Air Platforms

DTIC Thesaurus Topics

  • Air Force
  • Climate Change
  • Combustion
  • Diffraction
  • Electromagnetic Radiation
  • Flight Speeds
  • Heat Transfer
  • Light Sources
  • Phase Transformations
  • Raman Scattering
  • Raman Spectroscopy
  • Ramjet Engines
  • Refractive Index
  • Scattering
  • Supersonic Combustion Ramjet Engines
  • Three Dimensional
  • Two Dimensional

Fields of Study

  • Physics

Readers

  • Combustion and Flow Dynamics.
  • Organic Chemistry