MOTION OF A THIN AIRFOIL AT ARBITRARY DISTANCES FROM A SOLID AND A FLUID BOUNDARY.

Abstract

The aerodynamics of lifting systems flying at arbitrary distances from a boundary are discussed. The problem is solved by the kernel degeneration method through reduction of a singular equation of the first kind into a Fredholm equation of the second kind. The coefficients of the system of algebraic equations appearing in the solution of the Fredholm equation can be determined to any degree of accuracy by means of a computer. (Author)

Document Details

Document Type
Technical Report
Publication Date
Aug 27, 1969
Accession Number
AD0695984

Entities

People

  • B. S. Berkovskii
  • V. I. Koshevoi

Organizations

  • Johns Hopkins University Applied Physics Laboratory

Tags

DTIC Thesaurus Topics

  • Accuracy
  • Aerodynamics
  • Boundaries
  • Coefficients
  • Computers
  • Computing Devices
  • Equations
  • Fluid Dynamics
  • Fluid Mechanics

Fields of Study

  • Mathematics

Readers

  • Aerodynamics/Aeronautics.
  • Calculus or Mathematical Analysis