Induced Drag of Multiplanes Metadata

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Title

  • Main Title Induced Drag of Multiplanes
  • Series Title NACA Technical Notes

Creator

  • Author: Prandtl, L.
    Creator Type: Personal

Contributor

  • Originator: United States. National Advisory Committee for Aeronautics.
    Contributor Type: Organization
    Contributor Info: United States. National Advisory Committee for Aeronautics.

Date

  • Creation: 1924-02

Language

  • English

Description

  • Content Description: "The most important part of the resistance or drag of a wing system, the induced drag, can be calculated theoretically, when the distribution of lift on the individual wings is known. The calculation is based upon the assumption that the lift on the wings is distributed along the wing in proportion to the ordinates of a semi-ellipse. Formulas and numerical tables are given for calculating the drag. In this connection, the most favorable arrangements of biplanes and triplanes are discussed and the results are further elucidated by means of numerical examples" (p. 1).
  • Physical Description: [22] p. : ill.

Subject

  • Keyword: aircraft drag
  • Keyword: aerodynamics
  • Keyword: biplanes
  • Keyword: triplanes

Collection

  • Name: National Advisory Committee for Aeronautics Collection
    Code: NACA
  • Name: Technical Report Archive and Image Library
    Code: TRAIL

Institution

  • Name: UNT Libraries Government Documents Department
    Code: UNTGD

Rights

  • Rights Access: public
  • Rights License: pd
  • Rights Statement: No Copyright, Unclassified, Unlimited, Publicly available

Resource Type

  • Report

Format

  • Text

Identifier

  • Accession or Local Control No: 93R10254
  • OCLC: 1121049802
  • URL: http://digital.library.unt.edu/ark:/67531/metadc53856
  • Report No.: NACA-TN-182
  • Center for AeroSpace Information Number: 19930080964
  • Archival Resource Key: ark:/67531/metadc53856
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