The pressure distribution over a standard and a modified Navy elliptical wing tip on a biplane in flight Metadata

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Title

  • Main Title The pressure distribution over a standard and a modified Navy elliptical wing tip on a biplane in flight
  • Series Title NACA Technical Notes

Creator

  • Author: Rhode, Richard V.
    Creator Type: Personal

Contributor

  • Originator: Langley Memorial Aeronautical Laboratory
    Contributor Type: Organization
    Contributor Info: National Advisory Committee for Aeronautics. Langley Aeronautical Lab

Date

  • Creation: 1932-10

Language

  • English

Description

  • Content Description: "This note presents the results of flight pressure distribution tests on the right upper wing panel of a Douglas M-3 airplane equipped in turn with a standard Navy elliptical tip and a tip having the same plan form but modified in its front elevation from the swept-up aspect of the standard tip to a symmetrical aspect. The results are given in such form that the load distribution for any normal-force coefficient within the usual range encountered in flight may easily be determined. The results indicate that the modification in front elevation of the tip had no appreciable effect on the load distribution" (p. 1).
  • Physical Description: [33] p. : ill.

Subject

  • Keyword: pressure distributions
  • Keyword: Douglas D-3

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: 93R10504
  • URL: http://hdl.handle.net/2060/19930081214
  • Report No.: NACA-TN-433
  • Center for AeroSpace Information Number: 19930081214
  • Archival Resource Key: ark:/67531/metadc54102