AN ASYMPTOTIC METHOD FOR DETERMINING THE LIFT DISTRIBUTION OF A SWEPT-BACK WING OF FINITE SPAN

Abstract

A description is given of the flow about a flat, swept-back, symmetrically shaped airfoil which is moving with constant velocity V through a perfect ideal fluid filling three dimensional space. (Author)

Document Details

Document Type
Technical Report
Publication Date
May 01, 1964
Accession Number
AD0600422

Entities

People

  • James K. Thurber

Organizations

  • Adelphi University

Tags

DTIC Thesaurus Topics

  • Aircraft Wings
  • Airfoils
  • Airframes
  • Geometry
  • Mathematics
  • Mechanical Structure
  • Motion
  • Physical Properties
  • Sweptback Wings
  • Three Dimensional

Readers

  • Aerodynamics/Aeronautics.
  • Graph Algorithms and Convex Optimization.

Technology Areas

  • Space
  • Space - Space Objects