Some Factors Affecting the Stability and Performance Characteristics of Canard Aircraft Configurations Metadata

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Title

  • Main Title Some Factors Affecting the Stability and Performance Characteristics of Canard Aircraft Configurations
  • Series Title NACA Research Memorandums

Creator

  • Author: Spearman, M. Leroy
    Creator Type: Personal
  • Author: Driver, Cornelius
    Creator Type: Personal

Contributor

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

Date

  • Creation: 1958-06-23

Language

  • English

Description

  • Content Description: "A survey has been made of some of the factors to be considered in the design of canard aircraft configurations. The factors include Mach number and angle-of-attack effects as well as the effects of various geometric changes. Among the geometric variables included are the effects of wing plan form, wing height, wing twist, canard plan form, canard area, canard moment arm, forebody length, afterbody length, forebody deflection, vertical-tail plan form, vertical-tail size, vertical-tail location, and various ventral-fin arrangements" (p. 1).
  • Physical Description: 67 p. : ill.

Subject

  • Keyword: canard aircraft
  • Keyword: aircraft design

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: 93R19407
  • URL: http://hdl.handle.net/2060/19930090117
  • Report No.: NACA-RM-L58D16
  • Center for AeroSpace Information Number: 19930090117
  • Archival Resource Key: ark:/67531/metadc64195
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