THERMODYNAMIC COUPLING IN BOUNDARY LAYERS

Abstract

Experimental results gathered in recent years for binary mixture mass transfer models are shown to yield consistent evidence of discrepancies with analytic considerations. Specifically, measured recovery temperatures are appreciably higher than those predicted, while heat transfer coefficientsARE SATISFACTORILY REPRODUCED. It is shown on the basis of both approximate and exact solutions for plates and stagnation points that the discrepancies are related to thermal diffusion effects, a major influence being apparent in application of the surface boundary condition for an adiabatic wall. As a result, some reexamination is necessary of past criteria for mass addition effects as they pertain to specific injected media. A prime example is the equivalence of helium and air as coolants despite the heretofore suggested preference for low density injectants on a perfect gas basis. (Author)

Document Details

Document Type
Technical Report
Publication Date
Oct 01, 1961
Accession Number
AD0273308

Entities

People

  • Judson R. Baron

Organizations

  • Massachusetts Institute of Technology

Tags

DTIC Thesaurus Topics

  • Boundaries
  • Boundary Layer
  • Couplings
  • Diffusion
  • Heat Transfer
  • Layers
  • Low Density
  • Mass Transfer
  • Recovery
  • Stagnation Point
  • Thermal Diffusion

Readers

  • Combustion and Flow Dynamics.
  • Fluid Dynamics.
  • Theoretical Analysis.