A Method to Calculate the Parameters of Wings of Arbitrary Planform.

Abstract

The computation method developed in this thesis proceeds from the theory developed by Jones (Ref. 1). His final equations are first rewritten in matrix format. They are then organized into computational sequences that must be translated into computer programming language to calculate the aerodynamic parameters of wings of arbitrary planform.

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Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1984
Accession Number
ADA152689

Entities

People

  • E. M. Barber

Organizations

  • Naval Postgraduate School

Tags

Communities of Interest

  • Air Platforms
  • Materials and Manufacturing Processes

DTIC Thesaurus Topics

  • Aeronautics
  • California
  • Computational Science
  • Computer Programming
  • Computer Programs
  • Computers
  • Digital Computers
  • Engineering
  • Equations
  • Integral Equations
  • Language
  • Planform
  • Pressure Distribution
  • Programming Languages
  • Trailing Edges
  • Two Dimensional
  • United States

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Computer Science.