Three-Dimensional Subsonic Flows and Their Boundary Value Problems Extended to Higher Dimensions.

Abstract

In this paper, the steady, irrotational, subsonic flow of a gas around a given profile is studied in the case of arbitrary space dimension greater than two. We prove that the solution of this problem exists, is unique, and depends continuously on the incoming flow. This extends the previous results of Bers and of Finn and Gilbarg. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1981
Accession Number
ADA100597

Entities

People

  • Guang-chang Dong

Organizations

  • University of Wisconsin–Madison

Tags

Communities of Interest

  • Air Platforms
  • C4I

DTIC Thesaurus Topics

  • Boundaries
  • Boundary Value Problems
  • Equations
  • Euler Equations
  • Flow
  • Formulas (Mathematics)
  • Gas Flow
  • Inequalities
  • Integral Equations
  • Integrals
  • Intervals
  • Mathematics
  • Subsonic Flow
  • Three Dimensional
  • Two Dimensional
  • United States
  • Wisconsin

Fields of Study

  • Mathematics

Readers

  • Fluid Dynamics.
  • Systems Analysis and Design

Technology Areas

  • Space
  • Space - Hall-Effect Thruster