Condensation of H2O and D2O in Argon in the Centered Expansion Wave in a Shock Tube,

Abstract

Despite gasdynamic non-idealities in the flow produced in a shock tube, pressure measurements at three different locations in the driver section of the shock tube revealed that the expansion wave generated in relatively weak expansions could be viewed effectively as a simple centered expansion fan after an empirical shift of the actual origin of the expansion wave to a 'virtual' origin. The resulting centered expansion fan was used to study at two locations the condensation of H2O and D2O vapors in an excess of the carrier gas argon, with simultaneous pressure and light scattering measurements. The isentropic flow within the centered expansion fan was found to be preserved up to the point of the detectable onset of condensation by tailoring the onset conditions to occur at the tail of the expansion fan, thus rendering a simple analysis of the experiments possible. The onset conditions of H2O vapor were found to be in agreement with previous findings in supersonic nozzles and shock tubes, and they were well predicted by the so-called classical theory of homogeneous nucleation. The condensation of D2O vapor was found to exhibit similar trends as those of H2O vapor condensation despite the slight differences in physical properties between them due to isotopy. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1977
Accession Number
ADA035243

Entities

People

  • C. F. Lee

Organizations

  • Yale University

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Agreements
  • Boundary Layer
  • Equations
  • Fluids
  • Heat Energy
  • Light Scattering
  • Liquids
  • Measurement
  • New Jersey
  • Particles
  • Physical Properties
  • Pressure Measurement
  • Scattering
  • Shock Tubes
  • Supersonic Nozzles
  • United States
  • Water Vapor

Fields of Study

  • Physics

Readers

  • Calculus or Mathematical Analysis
  • Combustion Dynamics and Shock Wave Physics.
  • Combustion science or combustion engineering.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Boundary Layers
  • Hypersonics - Hypersonic Flow