Control Effectiveness Load and Hinge-Moment Characteristics of a Tip Control Surface on a Delta Wing at a Mach Number of 1.9 Metadata

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Title

  • Main Title Control Effectiveness Load and Hinge-Moment Characteristics of a Tip Control Surface on a Delta Wing at a Mach Number of 1.9
  • Series Title NACA Research Memorandums

Creator

  • Author: Conner, D. William
    Creator Type: Personal
  • Author: May, Ellery B., Jr.
    Creator Type: Personal

Contributor

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

Date

  • Creation: 1949-10-07

Language

  • English

Description

  • Content Description: Report presenting a wind-tunnel investigation of a semispan delta wing with the leading-edge swept back 60 degrees. A half-delta control surface was used and testing was performed with and without fences. Results regarding the rolling effectiveness, wing characteristics, and control-surface characteristics are provided.
  • Physical Description: 41 p. : ill.

Subject

  • Keyword: aircraft control
  • Keyword: aerodynamics

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: 93R15371
  • URL: http://hdl.handle.net/2060/19930086081
  • Report No.: NACA-RM-L9H05
  • Center for AeroSpace Information Number: 19930086081
  • Archival Resource Key: ark:/67531/metadc58388