Study of the Sub- and Supercritical Behavior of Fuel Droplets and Jets

Abstract

A project to conduct experiments to understand the flow and thermodynamic characteristics of liquid fuel droplets and jets in subcritical and supercritical environments was initiated. In the project initiation phase (Phase I), the literature on the subject matter was updated, the experimental setup was designed and modifications in the setup including installation of thermocouples, pressure transducers and analytical and diagnostic devices (LDV, PIV and high speed video imaging systems were either initiated or completed. Preliminary experiments on suspended and free falling hexane droplet gasification and combustion under subcritical and supercritical pressure conditions were undertaken. The preliminary results were very interesting and promising especially with respect to the variation of gasification rate with increasing pressure and decreasing droplet size and the effect of buoyancy on the burning droplet. The project remained slightly ahead of schedule at the end of the reporting period.

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Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1998
Accession Number
ADA353665

Entities

People

  • Tiejun Bai
  • Yaw D. Yeboah

Organizations

  • Clark Atlanta University

Tags

Communities of Interest

  • Human Systems
  • Space

DTIC Thesaurus Topics

  • Air Force
  • Air Force Research Laboratories
  • Chambers
  • Combustion
  • Combustion Chambers
  • Critical Temperature
  • Flow Rate
  • High Pressure
  • High Temperature
  • Literature
  • Materials Science
  • Measurement
  • Power Supplies
  • Pressure Transducers
  • Research Facilities
  • Stainless Steel
  • Thermocouples

Readers

  • Fluid Dynamics.
  • Fluid Mechanics and Fluid Dynamics.
  • Rocket Propulsion.