Wind-Tunnel Tests of a Hall High-Life Wing Metadata

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Title

  • Main Title Wind-Tunnel Tests of a Hall High-Life Wing
  • Series Title NACA Technical Notes

Creator

  • Author: Weick, Fred E.
    Creator Type: Personal
  • Author: Sanders, Robert
    Creator Type: Personal

Contributor

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

Date

  • Creation: 1932-05

Language

  • English

Description

  • Content Description: "Wind-tunnel tests have been made to find the lift, drag, and center-of-pressure characteristics of a Hall high-lift wing model. The Hall wing is essentially a split-flap airfoil with an internal air passage. Air enters the passage through an opening in the lower surface somewhat back of and parallel to the leading edge, and flows out through an opening made by deflecting the rear portion of the under surface downward as a flap. For ordinary flight conditions the front opening and the rear flap can be closed, providing in effect a conventional airfoil (the Clark Y in this case)" (p. 1).
  • Physical Description: [10] p. : ill.

Subject

  • Keyword: high-lift wings
  • Keyword: aircraft wings

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

  • OCLC: 1139565251
  • Report No.: NACA-TN-417
  • Center for AeroSpace Information Number: 19930081213
  • Archival Resource Key: ark:/67531/metadc54101
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