Hypersonic Attenuation in the Vicintiy of the Superfluid Transition of Liquid Helium

Abstract

The relative ultrasonic attenuation in liquid helium at 1 GHz has been measured in critical region with a fixed path interferometer. The sample was isolated from the main bath by a vacuum and the amplitude of the transmitted sound wave was measured while the temperature of the sample was made to drift at rates as slow as 3 x 10 to the minus 6th power K/sec. The attenuation is found to have a very large non-singular peak of about 2500/cm with its maximum at 3.26 plus or minus 0.20 mK below the lambda point. After the contribution of viscous and thermal losses to the attenuation has been subtracted, the temperature dependence of the critical attenuation is found to vary approximately as 1/th: square root of (T(p)-T) on both sides of T(p), the temperature of the peak. The attenuation peak cannot be explained by the Landau-Khalatnikov theory, and processes other than the decay of first into second sound must be considered. These results are in substantial agreement with earlier results but locate the peak with much greater reliability.

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Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1972
Accession Number
AD0744710

Entities

People

  • Daniel E. Commins

Organizations

  • University of California, Los Angeles

Tags

Communities of Interest

  • Energy and Power Technologies
  • Materials and Manufacturing Processes
  • Sensors

DTIC Thesaurus Topics

  • Acoustic Propagation
  • Acoustic Waves
  • Diagrams
  • Equations
  • Heat Energy
  • Measurement
  • Phase
  • Phase Diagrams
  • Phase Transformations
  • Sound Waves
  • Specific Heat
  • Thermal Conductivity
  • Transducers
  • Transition Temperature
  • Transitions
  • Vapor Pressure
  • Wave Propagation

Fields of Study

  • Physics

Readers

  • Materials Science and Engineering.
  • Quantum spin resonance or Electron Paramagnetic Resonance spectroscopy.
  • Thermal Physics or Thermal Science.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow