Movement of a Wing with a Small Aspect Ratio Near the Interface of Fluids with Different Densities,

Abstract

The problem of the movement of a wing with a small aspect ratio below a free fluid surface has been studied. The integral equation for a wing with a small aspect ratio moving above the interface of fluids with different densities was obtained in a similar manner. But these studies did not determine the distribution of the load over the wing chord. This report will solve the problem which makes it possible to find the load distribution over the wing chord when condition lambda F r squared approaches zero, is satisfied, the Froude number being calculated for the wing span.

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Document Details

Document Type
Technical Report
Publication Date
Jan 31, 1977
Accession Number
ADA045921

Entities

People

  • S. I. Putilin

Organizations

  • National Air and Space Intelligence Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Accuracy
  • Air Force
  • Aspect Ratio
  • Asymptotic Series
  • Equations
  • Foreign Technology
  • Froude Number
  • Graphics
  • Integral Equations
  • Integrals
  • Load Distribution
  • Standards
  • Trailing Edges
  • Translations

Readers

  • Aerodynamics/Aeronautics.
  • Atmospheric Science / Meteorology, specifically Wind Wave Turbulence.
  • Calculus or Mathematical Analysis