Condensation of Carbon Dioxide in Supersonic Nozzles

Abstract

Test results indicate a definite region of supersaturation of CO2 prior to its expansion. In Curve I, using assumed isentropic temperatures based on measured pressure ratio, the supersaturation ratio (ratio of static pressure to flat-surface equilibrium pressure at local temperature) obtains an estimated value of 9.14, prior to condensation occurring. In Curve 3, the supersaturation ratio reaches a value of 10.5 prior to condensation and in Curves 4, 5 and 7 values of 11.6, 13.4 and 16.8, respectively. The fact that supersaturation ratios steadily increase prior to the occurrence of rapid condensation tends to support the predicitions of nucleation theory that, for CO2, the lines of constant nucleation rate diverge with decreasing pressure and temperatures and that nucleation rates have a critical value of the ratio between the static and stagnation pressures beyond which they rise astronomically, creating a narrow zone where the large portion of condensation occurs. It is further concluded that the interferometer does not lend itself to the convenient procurement of accurate density and pressure profiles in this particular nozzle under these extreme temperature conditions.

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Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1964
Accession Number
AD0608161

Entities

People

  • Karl M. Duff

Organizations

  • Massachusetts Institute of Technology

Tags

Communities of Interest

  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Boundary Layer
  • Chemistry
  • Equations
  • Heat Energy
  • Heat Of Vaporization
  • Heat Transfer
  • Interferometers
  • Latent Heat
  • Layers
  • Measurement
  • Physics
  • Pressure Gages
  • Pressure Measurement
  • Refractive Index
  • Specific Heat
  • Stagnation Pressure
  • Supersonic Nozzles

Readers

  • Combustion and Flow Dynamics.
  • Economics
  • Materials Science and Engineering.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow