Stability Analysis of the Compressible, Adiabatic, Similar Boundary Layer Equations (Lower Branch).

Abstract

In a previous report, the authors analyzed the stability of the lower branch solutions of the incompressible (M sub infinity = 0) Falkner-Skan boundary layers. This report extends this work by including the effect of Mach number M sub infinity on the stability of adiabatic case. (Author)

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Document Details

Document Type
Technical Report
Publication Date
May 01, 1981
Accession Number
ADA108507

Entities

People

  • G. R. Verma
  • S. J. Scherr
  • W. L. Hankey

Organizations

  • University of Rhode Island

Tags

Communities of Interest

  • Energy and Power Technologies
  • Materials and Manufacturing Processes

DTIC Thesaurus Topics

  • Acoustic Propagation
  • Air Force
  • Air Force Facilities
  • Boundaries
  • Boundary Layer
  • Boundary Layer Flow
  • Equations
  • Flow
  • Heat Transfer
  • Mach Number
  • Navier Stokes Equations
  • Pressure Gradients
  • Scientific Research
  • Specific Heat
  • Thermal Conductivity
  • Three Dimensional
  • Two Dimensional

Readers

  • Fluid Dynamics.