Regularization of the Singular Integral Equation for a Wing in an Unsteady Subsonic Gas Flow

Abstract

This study attempts to regularize the singular integral equation for a wing in an unsteady subsonic plane-parallel gas flow in acceleration potential space, obtain the Fredholm equation for determining the distribution function gamma(xi), and find the asymptotic solution.

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Document Details

Document Type
Technical Report
Publication Date
Feb 07, 1977
Accession Number
ADA044670

Entities

People

  • Yu. A. Abramov

Organizations

  • National Air and Space Intelligence Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Abstracts
  • Air Force
  • Bibliographies
  • Classification
  • Compressible Flow
  • Differential Equations
  • Distribution Functions
  • Equations
  • Flow
  • Fluid Flow
  • Foreign Technology
  • Gas Flow
  • Identities
  • Incompressible Flow
  • Integral Equations
  • Integrals
  • Security

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Calculus or Mathematical Analysis
  • Fluid Dynamics.

Technology Areas

  • Space
  • Space - Hall-Effect Thruster