Systematic Investigations of the Effects of Plan Form and Gap between the Fixed Surface and Control Surface on Simple Flapped Wings Metadata

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Title

  • Main Title Systematic Investigations of the Effects of Plan Form and Gap between the Fixed Surface and Control Surface on Simple Flapped Wings
  • Series Title NACA Technical Memorandums

Creator

  • Author: Goethert
    Creator Type: Personal
  • Author: Roeber
    Creator Type: Personal

Contributor

  • Originator: Zentrale fuer Wissenschaftliches Berichtswesen
    Contributor Type: Organization

Date

  • Creation: 1949-05-01

Language

  • English

Description

  • Content Description: Four component measurements of 12 wings of symmetric profile having flaps with chord ratios t(sub R)/t(sub L) = 0.3 and t(sub R)/t(sub L) = 0.2 are treated in this report. As a result of the investigations, the effects of plan form and gap between fixed surface and control surface have been clarified. Lift, drag, pitching moment, and hinge moment were measured in the control-surface deflection range: -23 deg < or = beta < or = 23 deg and the range of angle of attack: -20 deg < or = alpha < or = 20 deg. Six wings with flaps of small chord (t(sub R)/t(sub L) < 0.1) were investigated at large flap settings.

Subject

  • Keyword: aerodynamics

Source

  • ZWB Forschungsbericht; Rept-552/4

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

  • URL: http://hdl.handle.net/2060/20050019655
  • Report No.: NACA-TM-1206
  • Center for AeroSpace Information Number: 20050019655
  • Archival Resource Key: ark:/67531/metadc64486