The Flow of a Compressible Fluid Past a Sphere

Abstract

The flow of a compressible fluid past a sphere fixed in a uniform stream is calculated to the third order of approximation by means of the Janzen-Rayleigh method. The velocity and the pressure distributions over the surface of the sphere are computed and the terms involving the fourth power of the Mach number, neglected in Rayleigh's calculation, are shown to be of considerable importance as the local velocity of sound is approached on the sphere. The critical Mach number, that is, the value of the Mach number at which the maximum velocity of the fluid past the sphere is just equal to the local velocity of sound, is calculated for both the second and third approximations and is found to be, respectively, M sub cr = 0.587 and M sub cr = 0.573.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
May 01, 1940
Accession Number
ADA801328

Entities

People

  • Carl Kaplan

Organizations

  • National Advisory Committee for Aeronautics

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aeronautical Laboratories
  • Aeronautics
  • Boundaries
  • Equations
  • Equations Of Motion
  • Flow
  • Lepidoptera
  • Mach Number
  • Molecular Dynamics
  • Potential Flow
  • Pressure Distribution
  • Specific Heat

Fields of Study

  • Physics

Readers

  • Adaptive Control and Estimation with Uncertainty in Dynamic Systems.
  • Fluid Mechanics and Fluid Dynamics.