Low-speed lateral control characteristics of an unswept wing with hexagonal airfoil sections and aspect ratio 4.0 at a Reynolds number of 6.2 x 10(exp 6) Metadata

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Title

  • Main Title Low-speed lateral control characteristics of an unswept wing with hexagonal airfoil sections and aspect ratio 4.0 at a Reynolds number of 6.2 x 10(exp 6)
  • Series Title NACA Research Memorandums

Creator

  • Author: Hadaway, William M.
    Creator Type: Personal

Contributor

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

Date

  • Creation: 1953-03-20

Language

  • English

Description

  • Content Description: Report presenting a lateral-control investigation in the 19-foot pressure tunnel of an unswept wing with 6-percent-thick hexagonal airfoil sections, aspect ratio 4.0, and taper ratio 0.625. The wing was mounted on a circular fuselage with a fineness ratio of 10 to 1.
  • Physical Description: 24 p. : ill.

Subject

  • Keyword: aircraft control
  • Keyword: airfoils

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: 93R16806
  • URL: http://hdl.handle.net/2060/19930087516
  • Report No.: NACA-RM-L53A29
  • Center for AeroSpace Information Number: 19930087516
  • Archival Resource Key: ark:/67531/metadc59561
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