Flow Separation.

Abstract

The calculation of laminar separation has always represented one of the most relevant problems of boundary layer theory, even within the classical Prandtl's assumption of vanishing transverse pressure gradients. However, the validity of this assumption is in question not only in certain problems of supersonic separation where the classical theory cannot provide an answer, but also in the simplest incompressible problems. Recent theories attempting to calculate separation after relaxing Prandtl's assumption are reveiwed in this paper. Purely numerical results based on the finite difference solution of the complete Navier-Stokes equations were considered to be beyond the scope of this review and are just briefly mentioned. An analytical procedure based on multiple layer treatment is discussed. A third procedure of interest is the generalization of von Karman momentum integral procedure taking into account the existence of transverse pressure gradients.

Document Details

Document Type
Technical Report
Publication Date
Feb 01, 1976
Accession Number
ADA025662

Entities

People

  • Luigi Crocco

Organizations

  • AGARD

Tags

DTIC Thesaurus Topics

  • Boundary Layer
  • Computational Science
  • Equations
  • Flow Separation
  • Fluid Dynamics
  • Fluid Mechanics
  • Layers
  • Navier Stokes Equations
  • Pressure Gradients
  • Transverse

Fields of Study

  • Physics

Readers

  • Fluid Dynamics.
  • Systems Analysis and Design

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flight