A METHOD OF CALCULATING THREE-DIMENSIONAL LAMINAR BOUNDARY LAYERS OF STEADY COMPRESSIBLE FLOWS,

Abstract

A numerical method of calculating the laminar boundary layer on any three-dimensional surface in steady compressible flow is presented. This method can be applied readily on an automatic digital computer with any desired accuracy. It is valid at and near the usual singular points and lines of a surface as well as elsewhere. A principle clarifying various aspects of three-dimensional flow also is given. (Author)

Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1957
Accession Number
AD0821759

Entities

People

  • G. S. Raetz

Tags

DTIC Thesaurus Topics

  • Accuracy
  • Automatic
  • Boundaries
  • Boundary Layer
  • Compressible Flow
  • Computers
  • Digital Computers
  • Flow
  • Laminar Boundary Layer
  • Layers
  • Three Dimensional
  • Three Dimensional Flow

Fields of Study

  • Physics

Readers

  • Computer Science/Computer Engineering/Data Science/Digital Signal Processing.
  • Fluid Dynamics.