Stability of Liquid Films Adjacent to Compressible Streams,

Abstract

An analysis is presented for the linear stability of a liquid film adjacent to a compressible viscous gas stream. The analysis is valid for all wavelengths and liquid Reynolds numbers. The pressure and shear perturbations exerted by the gas on the liquid are calculated using a gas model which takes into account the gas viscosity, velocity profile, and heat transfer. The results show that an inviscid uniform stream model for the gas is inadequate unless the disturbed boundary layer is very thin. Although the present linear analysis is in fairly good agreement with the experimental observations for subsonic flow, it does not predict the observed wavelengths and wave speeds for supersonic flow. (Author)

Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1973
Accession Number
AD0758982

Entities

People

  • Ali Hasan Nayfeh
  • Gary L. Bordner
  • William S. Saric

Organizations

  • Virginia Tech

Tags

DTIC Thesaurus Topics

  • Agreements
  • Boundaries
  • Boundary Layer
  • Flow
  • Fluid Dynamics
  • Fluid Flow
  • Heat Transfer
  • Layers
  • Observation
  • Perturbations
  • Reynolds Number
  • Subsonic Flow
  • Supersonic Flow
  • Viscosity

Fields of Study

  • Physics

Readers

  • Fluid Dynamics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow