Evaporation of Monodisperse Fuel Sprays in Flowing Air.

Abstract

This work represents the Final Report of a research program dealing with liquid fuel droplet evaporation in flowing high temperature and pressurized air. A major effort was applied to the design, fabrication, and utilization of a heated air flow tunnel into which monodisperse droplets with controlled axial spacing and velocity it was possible to photomicroscopy to measure the droplets (typically 100 um) along individual spray streams, and then to calculate an effective evaporation rate. Both n-heptane and JP-4 fuels were injected into a hto air stream with air velocities typically exceeding 5 m/sec. The droplet evaporation data show that, for our spray, the quasi-steady isolated drop theory underestimates the evaporation rate. Air velocity and turbulence were measured by an LDV system and the recirculation zone downstream of the injector was precisely measured under cold and hot flow. These data, with the measured droplet evaporation, were sufficient in scope to allow a comparison of measurements with a comprehensive turbulent flow model. Results of that modeling work are presented and indicate that there is excellent agreement between analysis and measured flow conditions.

Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1986
Accession Number
ADA177119

Entities

People

  • G. N. Schroering
  • H. Krier
  • J. E. Kirwan
  • J. E. Peters
  • Keehoon Kim

Organizations

  • University of Illinois Urbana–Champaign

Tags

DTIC Thesaurus Topics

  • Agreements
  • Air Flow
  • Evaporation
  • Fabrication
  • Flow
  • Fluid Dynamics
  • Fluid Flow
  • Fuel Sprays
  • Fuels
  • High Temperature
  • Injectors
  • Measurement
  • Sprays
  • Transition Temperature
  • Turbulent Flow

Readers

  • Aerosol Science/Aerosol Physics
  • Fluid Mechanics and Fluid Dynamics.
  • Technical Research and Report Writing.

Technology Areas

  • Space
  • Space - Hall-Effect Thruster