The Field of a Uniform Circular Source Disk,

Abstract

The flow field of a ducted propeller can be calculated by means of flow singularities. An important part of the method is a sink disk which simulates an infinitely bladed propeller in a steady inviscid incompressible flow. The field around a circular disk uniformly covered with a surface source distribution is tabulated to four decimal accuracy.

Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1961
Accession Number
AD0734102

Entities

People

  • I. Fleischer
  • L. Meyerhoff

Tags

DTIC Thesaurus Topics

  • Accuracy
  • Engineering
  • Flow
  • Flow Fields
  • Incompressible Flow
  • Propellers
  • Shrouded Propellers

Readers

  • Aerospace Engineering
  • Fluid Dynamics.