AIR AND NITROGEN CONDENSATION IN HYPERSONIC NOZZLE FLOW,

Abstract

Earlier experimental air condensation results were extended to lower pressures and higher Mach numbers where it was found that air behaves essentially as pure nitrogen and large amounts of supercooling are obtained. A theoretical analysis, based on established drop growth and self-nucleation concepts, supported the experimental findings. A correlation parameter governing the onset of condensation is presented. The analysis indicated that at the higher static pressures, where little or no supercooling is observed experimentally, the seemingly negligible amounts of CO2 and H2O in the wind tunnel air are sufficient to cause O2 and N2 condensation through a seeding action. A new method is presented for determining a conservative value of minimum stagnation temperature for obtaining condensation-free hypersonic flow. (Author)

Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1967
Accession Number
AD0657772

Entities

People

  • Fred L. Daum
  • George Gyarmathy

Organizations

  • Air Force Research Laboratory

Tags

DTIC Thesaurus Topics

  • Condensation
  • Flow
  • Hypersonic Flow
  • Hypersonic Nozzles
  • Mach Number
  • Nitrogen
  • Nozzles
  • Nucleation
  • Physical Properties
  • Stagnation Temperature
  • Static Pressure
  • Supercooling
  • Transition Temperature
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Combustion and Flow Dynamics.
  • Theoretical Analysis.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flight
  • Hypersonics - Hypersonic Flow