On Two-Dimensional Supersonic Flows

Abstract

In previous reports by the author, the method of operators has been applied to the investigation of two-dimensional irrotational flow patterns of an ideal compressible fluid, mostly in the subsonic case. Using a similar approach in the present paper, the author defines two different operators which generate supersonic two-dimensional flow patterns from differentiable functions of one real variable (An operator is any rule by means of which one function is converted into another. This concept is discusses in some detail in the body of this paper.) Since operators of the type considered preserve many properties of the functions to which they are applied and since the theory of functions of one real variable is more extensively developed than that of solutions of the compressibility equations, the results obtained can be used as a basis for the investigation of supersonic flow patterns.

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Document Details

Document Type
Technical Report
Publication Date
May 01, 1949
Accession Number
ADA380623

Entities

People

  • Stefan Bergman

Organizations

  • Brown University

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Analytic Functions
  • Complex Variables
  • Compressible Flow
  • Computational Fluid Dynamics
  • Computational Science
  • Differential Equations
  • Equations
  • Fluid Dynamics
  • Fluid Flow
  • Incompressible Flow
  • Linear Differential Equations
  • Mach Number
  • Partial Differential Equations
  • Real Variables
  • Subsonic Flow
  • Supersonic Flow
  • Two Dimensional

Fields of Study

  • Mathematics

Readers

  • Fluid Dynamics.
  • Linear Algebra

Technology Areas

  • Hypersonics